Bowersox Group Publications

^* students under the direction of Dr. Bowersox.

Publications

1. Baranwal, A., Donzis, D., Bowersox, R., “Mach Number and Wall Thermal Boundary Condition Effects on Near-Wall Compressible Turbulence,” Journal of Fluid Mechanics, in-review, 2023.
2. Siddiqui, F. Ledbetter, S., Shine,^*, Bowersox, R., Gragston, M., “Correlated Off-Body Density Fluctuations and Surface Heating in Hypersonic Boundary Layer Transition,” Experiments in Fluids, Accepted, 2023.
3. Siddiqui, F., Gragston, M, Bowersox, R., “Optical Measurements of Nonlinear Mack Mode Interactions on a Cooled Flared Cone in Quiet Mach 6 Flow,” Accepted AIAA SCITECH 2024.
4. Meritt, R., Molinaro, N., Dufrene, A., MacLean, M., Bowersox, R., “A Comparative Analysis of In-Flight and Full-Scale Ground Facility Wall Shear Measurements on the BOLT II Vehicle,” Accepted AIAA SCITECH 2024.
5. Ledbetter, S., Siddiqui, F., Shine, ^*, Bowersox, R., “Correlating Surface Heat Transfer Rates and Off-Body Spectral Measurements in Roughness Dominated Hypersonic Boundary Layer Transition,” Accepted AIAA SCITECH 2024.
6. Smith, C., Siddiqui, F., Ledbetter, S., Gragston, M., Shine,^*, Ibanez, O., McGruder,^* D., Bowersox, R., “Measurements of Surface Heating from Hypersonic Boundary Layer Transition by Simultaneous Temperature-Sensitive Paint and Infrared Thermography,” Accepted AIAA SCITECH 2024.
7. Dean, ^*, Pehrson, J., Bowersox, R., Dogariu, “Expansion Tunnel Freestream Characterization Using Ultrafast Diagnostics,” Accepted AIAA SCITECH 2024.
8. Feltiz, S., Zhang, Z., Dean,^*, Bowersox, R., Siddiqui, F., Gragston, M., “Measurements of NO Rotational and Vibrational Temperatures Behind a Normal Shock in Hypervelociy Flow,” Accepted AIAA SCITECH 2024.
9. Broslawski, ^*, Britt, A., North, S., Bowersox, R., “The Characterization of a DC Glow Discharge in a Tripped Hypersonic Boundary Layer,” Accepted, AIAA SCITECH 2024.
10. Broslawski,^*, Buen, Z, Britt, A., Smotzer, M., North, S., Bowersox, R., “The Characterization of Thermal Nonequilibrium in a Hypersonic Turbulent Boundary Layer,” Accepted, AIAA SCITECH 2024.
11. Smotzer, M., Buen, Z., Broslawski,^*, Britt, A., Morreale,^* B., North, S., Bowersox, R., “Nitric Oxide Planar Laser Induced Fluorescence Rotational Thermometry Characterization of a Hypersonic Boundary Layer,” Accepted, AIAA SCITECH 2024.
12. Pehrson, C., Leonov, B., Melone,^*, Lakebrink, M., Bowersox, R., Miles, R., Limbach, C., “Hypersonic FLEET velocimetry and uncertainty characterization in a tripped boundary layer,” Measurement Science and Technology, Accepted, 2023 (online 10.1088/1361-6501/acf592).
13. Leonov, B., Dean,^* Limbach, C., Bowersox, R., Miles, R., “”High-Speed Planar Laser-Induced Fluorescence Investigation of Nitric Oxide Generated by Hypersonic Mach Reflections for Computational Fluid Dynamics Validation,” Physics of Fluids, Vol. 35, June, 2023, pp. 066102-1-17.
14. Wirth,^*, Morreale,^* B., Bowersox, R., Wheaton, B., “Boundary Layer Turbulence Flight Experiment in Memory of Mike Holden: Side A Flight Data 2,” AIAA-2023-3440, AIAA AVIATION, June, 2023.
15. Merritt, R., Molinaro, N., Dufrene, A., and Bowersox, R., “A Summary of AFOSR BOLT II Direct Wall Shear Stress,” AAIAA-2023-3452, IAA AVIATION, June 2023.
16. Leonov, B., Dean,^*, McGruder,* D., Limbach, C., Bowersox, R., Miles, R., “Burst-mode Nitric Oxide PLIF for Visualization and Mode Spectral Analysis of Hypersonic Shear Layer,” AIAA-2023-4383, AIAA AVIATION, June, 2023.
17. Wirth,^*, Kocian, T., Vaughn, J., Reed, H., White, E., Bowersox, R., “Preliminary Investigations of Shock-Boundary Layer Interactions on the High-Speed Army Reference Vehicle,” JANNAF, Paper No. 8938, May, 2023.
18. Wirth,^*, Kocian, T., Vaughn, J., Reed, H., White, E., Bowersox, R., Lakin,^* G., “Transient Heat Flux During Dynamic Pitch and Roll of the High-Speed Army Reference Vehicle in a Wind Tunnel,” JANNAF, Paper No. 8939, May, 2023.
19. Kostak-Teplicek,^*, Bowersox, R., “Hypersonic Stability and Breakdown Measurements on the AFRL/AFOSR BOLT II Geometry,” AIAA-2023-0085, SCITECH Forum, Jan. 2023.
20. Carlson,^*, Bowersox, R., Tichenor, N., “Numerical Simulation of Supersonic Turbulent Boundary Layers Subjected to Favorable Pressure Gradients,” AIAA-2023-1229, SCITECH Forum, Jan. 2023.
21. Wirth,^*, Morreale,^* B, Kostak-Teplicek,^* H., Bowersox, R., Dufrene, A., Portoni, P., Wadhams, T., “Boundary Layer Turbulence Flight Experiment in Memory of Mike Holden: Side A Flight Data,” AIAA-2023-0862, SCITECH Forum, Jan. 2023.
22. Dufrene, A., Portoni, P., Wadhams, T., Kostak-Teplicek,^*, Bowersox, R., “Boundary Layer Turbulence Flight Experiment in Memory of Mike Holden: Vehicle Design, Instrumentation, and Ground Test Results,” AIAA-2023-0478, SCITECH Forum, Jan. 2023.
23. Morreale,^*, Swinny,^* E., Kostak-Teplicek,^* H., Bowersox, R., White, E., Dufrene, A., Wadhams, T., Popkin, S., Adamczak, D., Tancred, T., “Boundary Layer Turbulence Flight Experiment in Memory of Mike Holden: Pre-Flight Mission Design,” AIAA-2023-0477, SCITECH Forum, Jan. 2023.
24. Morreale,^*, Shine,^* J., Bowersox, R., Bitter, N., Wagnild, R., “ Hypersonic Multi-Fidelity Turbulence Modeling on Mach 5 Blunt Ogive with Cool Walls,” AIAA-2023-0455, SCITECH 2023.
25. Shine,^*, White. J., Bowersox, R., White, E., Gragston, M., Siddiqui, F., “3D-Printed Quasi-Random Distributed Roughness for Turbulent Boundary Layer Analysis on Hypersonic Ogive Nosecones,” AIAA-2023-0660, SCITECH Forum, Jan. 2023.
26. Bryan,^*, Dean,^* T., Morreale,^* B., Bowersox, R., “Computational Simulations of Hypersonic Mach Stems at High Enthalpy,” AIAA-2023-0858, SCITECH Forum, Jan. 2023.
27. Baranwal, A., Donzis, D., Bowersox, R., “Turbulent Heat Flux in Supersonic Flow for Different Thermal Boundary Conditions,” AIAA-2023-0868, SCITECH Forum, Jan. 2023.
28. Siddiqui, F., Gragston, M., Shine,^*, Bowersox, R., “Measurements of the Evolution of Scalar Disturbance Spectra and Heat Transfer Rates on a Flared Cone at Mach 6,” AIAA-2023-1988, SCITECH Forum, Jan. 2023.
29. Dean,^*, Siddiqui, F., Gragston, M., Bowersox, R., “Index of Refraction Fluctuation Spectra in Aerothermochemical Non-equilibrium Shock Layers,” AIAA-2023-0270, SCITECH Forum, Jan. 2023.
30. Siddiqui, F., Gragston, M., Bowersox, R., “Measurement of Wall-Cooling Effects on Hypersonic Boundary-Layer Transition Using Focused Laser Differential Interferometry,” AIAA Journal, Vol. 60, No. 11, 2022, pp. 6214-6224.
31. Vasile, J., Fresconi, F., DeSpirito, J., Duca, M., Recchia, T., Grantham, B., Bowersox, R., White, E., “High-Speed Army Reference Vehicle,” ARL-TN-1128, Aug. 2022.
32. Wirth,^*, Bowersox, R., “Tunnel Environment Effects on the Single Fin-Cone at Mach 6,” AIAA 2022-4137, AVIATION Forum, June, 2022.
33. Dean,^*, Blair,^* T., Roberts,^* M., Limbach, C., Bowersox, R., “On the Initial Characterization of a Large-Scale Hypervelocity Expansion Tunnel,” AIAA-2022-1602, SCITECH Forum, Jan. 2022.
34. Limbach, C., Melone,^*, Pehrson, J., Miles, R., Bowersox, R., Lakebringk, M., Bowcutt, K., “Design and Evaluation of an Optically Accessible Canonical Inlet Model for CFD-Validation Experiments,” AIAA-2022-0067, SCITECH Forum, Jan. 2022.
35. Lukasik, G., Rogers, J., Kota, K., Bowersox, R., Lacy, T., Kulatilaka, W., “Ultra-Highspeed Optical Diagnostics of Water Droplet Impact, Breakup, and Shock Boundary Layer Interactions of Hypervelocity Projectiles,” AIAA-2022-1656, SCITECH Forum, Jan. 2022.
36. Nicholson, G., Haung, J., Duan, L., Choudhari, M., Morreale,^*, Bowersox, R., Nicholson, G., Duan, L., “Budgets of Reynolds Stresses and Turbulent Heat Flux for Hypersonic Turbulent Boundary Layer Subject to Pressure Gradients,” AIAA-2022-1059, SCITECH Forum, Jan. 2022.
37. Siddiqui,^*, Gragston, M., Bowersox, R., “Focused Laser Differential Interferometry on a Cooled Flared Cone at Mach 6,” AIAA-2022-1825, SCITECH Forum, Jan. 2022.
38. Broslawski,^*, Morreale,^* B., Bowersox, R., Nicholson, G., Duan, L., “Further Validation and Implementation of an Algebraic Energy Flux Model for High-Speed Gaseous Flows,” AIAA-2022-0340, SCITECH Forum, Jan. 2022.
39. Baranwal, A, Donzis, D., and Bowersox, R., “Asymptotic Behavior at the Wall in Compressible Turbulent Channels,” Journal of Fluid Mechanics, Vol. 933, 2021, pp. A28.1-13.
40. Siddiqui,^*, Gragston, M., Saric, W., and Bowersox, R., “Second-Mode Instabilities on a Cooled Flared Cone with Discrete Roughness Elements at Mach 6,” Experiments in Fluids, Vol. 62, No. 10, 2021, pp. 213.1-13.
41. Leidy,^*, Neel,^* I., Tichenor, N., Bowersox, R., and Schmisseur, J., “Tunnel Noise Effects on Hypersonic Cylinder-Induced Transitional Shock Wave Boundary Layer Interactions,” AIAA Journal, Vol. 59, No. 7, 2021, pp. 2357-2367.
42. McManamen,^*, Donzis, D., North, S., and Bowersox, R., “Velocity and Temperature Fluctuations in a High Speed Shock-Turbulence Interaction,” Journal of Fluid Mechanics, Vol. 913, 2021, pp. A10.1-28.
43. Hutchinson,^* and Bowersox, R., “A Sonic Boom Propagation Code for Studying Atmospheric Effects and Uncertainties,” AIAA-2020-0010, AIAA SCITECH Forum, Jan. 2021.
44. Siddiqui,^*, Saric, W., Bowersox, R., “Interaction of Second-Mode Disturbances and 3-D Roughness on a Cooled Flared Cone at Mach 6,” AIAA-2020-1092, AIAA SCITECH Forum, Jan. 2021.
45. Nicholson, G., Huang, J., Duan, L., Choudhari, M., Bowersox, R., “Simulation and Modeling of Hypersonic Turbulent Boundary Layers Subject to Favorable Pressure Gradients due to Streamline Curvature,” AIAA-2021-1672, AIAA SCITECH Forum, 2021.
46. Radespiel, R., Ali, C., Bowersox, R., Leidy,^*, Tanno, H., Kirk, L, Reshotko, E., “Chapter 9 – Experimental Investigation of Roughness Effects on Transition on Blunt Spherical Capsule Shapes,” in Hypersonic Boundary-Layer Transition Prediction, NATO STO Technical Report TR-AVT-240, Co-Chairs R. Radespiel, S. Schneider, Neuilly-sur-Seine Cedex, France, Aug. 2020, pp. 9.1-9.30. ISBN 978-92-837-2227-4.
47. Leidy,^*, Neel,^* I., Tichenor, N., Bowersox, R., “High-Speed Schlieren Imaging of Cylinder-Induced Hypersonic-Shock-Wave–Boundary-Layer Interactions,” AIAA Journal, Vol. 58, No. 7, 2020, pp. 3090-3099.
48. Kostak,^* and Bowersox, R., “ Pre-Flight Ground Test Analyses of the Boundary Layer Transition (BOLT) Flight Geometry,” J. Spacecraft and Rockets, Vol. 58, No. 1., 2021, pp. 67-77.
49. Dwivedi, A., Broslawski,^*, Candler, G., and Bowersox, R., “Three-dimensionality in Shock/Boundary Layer Interactions: A Numerical and Experimental Investigation,” AIAA-2020-3011, AIAA AVIATION Forum 2020, June 2020.
50. Kostak,^*, Bowersox, R., “Hypersonic Boundary Layer Off-Body and Surface Measurements on the AFOSR BOLT,” AIAA-2020-1043, AIAA SCITECH Forum, Jan. 2020.
51. Baranwal, A., Donzis, D., and Bowersox, R., “Vibrational Turbulent Prandtl Number in Flows with Thermal Non-Equilibrium,” AIAA-2020-2052, AIAA SCITECH Forum, 2020.
52. Buen, Z., Broslawski,^*, Smotzer, M., Kuszynski, J., North, S., Bowersox, R., “Towards Vibrationally Excited Nitric Oxide Monitoring (VENOM) in a Laminar, Hypersonic Boundary Layer,” AIAA-2020-1275, AIAA SCITECH Forum,Jan. 2020.
53. Carlson,^*, Bowersox, R., Tichenor, N., “Proper Orthogonal Decomposition Analysis of Hypersonic Turbulent Boundary Layers Subjected to Streamline Wall Curvature, AIAA-2020-2060, AIAA SCITECH Forum, Jan. 2020.
54. Chen, C., Donzis, R., Bowersox, R., “Characteristic Locations in Shock- Turbulence Interaction,” AIAA-2020-1812, AIAA SCITECH Forum, 2020.
55. Schmisseur, J., Bowersox, R., Combs. C., Coder, J., Gragston, M., Glasby, R., “Low-Frequency Unsteadiness in Transitional Shock/Boundary Layer Interactions (Invited),” Oral presentation, AIAA SCITECH Forum, 2020.
56. Leidy,^*, Neel,^* I., Tichenor, N., Bowersox, R., Schmisseur, J., “Some effects of tunnel noise on cylinder-induced Mach 6 transitional shock wave boundary layer interactions,” AIAA-2020-0582, AIAA SCITECH Forum, Jan. 2020.
57. Huang, J., Nicholson, G., Duan, L., Choudhari, M., Bowersox, R., “Simulation and Modeling of Cold-Wall Hypersonic Turbulent Boundary Layers on a Flat Plate,” AIAA-2020-0571, AIAA SCITECH Forum, 2020.
58. Winner, J., North, S., Bowersox, R., “Applicability of the Invisible Ink Vibrationally Excited Nitric Oxide Monitoring Technique to Various Flow Conditions: A Temperature Perturbation Simulation Study,” Applied Optics, Vol. 58, No. 10, 2019, pp. 2702-2712.
59. Radespiel, R., Ali, C., Bowersox, R., Leidy,^*, Tanno, H., Kirk, L, Reshotko, E., “Experimental Investigation of Roughness Effects on Transition on Blunt Spherical Capsule Shapes,” AIAA Journal Spacecraft and Rockets, Vol. 56, No. 2, 2019, pp. 405-420.
60. Kostak,^*, Bowersox, R., McKiernan, G., Thome, J., Candler, G., King, R., “Freestream Disturbance Effects on Boundary Layer Instability and Transition on the AFOSR BOLT Geometry,” AIAA-2019-0088, AIAA SCITECH Forum, January 2019.
61. Paul, A., West, N., Winner, J., Bowersox, R., North, S., and Hase, W., “Non-Statistical Intermolecular Energy Transfer from Vibrationally Excited Benzene in a Mixed Nitrogen-Benzene Bath,” Journal of Chemical Physics, 2018, Vol. 149, 134101.
62. Leidy,^*, Neel,^* I., Tichenor, N., Bowersox, R., “Cylinder-Induced Hypersonic Transitional Shock Wave Boundary Layer Interactions: Pressure Fluctuations and Thermal Loading,” AIAA-2018-5074, 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference, Sept. 2018.
63. Neel,^*, Leidy,^* A., Tichenor, N., Bowersox, R., “Characterization of Environmental Disturbances on Hypersonic Crossflow Instability on the HIFiRE-5 Elliptic Cone,” AIAA-2018-5375, 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference, Sept. 2018.
64. Leidy,^*, Neel,^* I., Tichenor, N., Bowersox, R., J. Schmisseur, “High Speed Schlieren Imaging and Hotwire Characterization of Cylinder-Induced Hypersonic Shock Boundary Layer Interactions,” AIAA-2018-3703, AIAA AVIATION, June 2018.
65. Leidy,^*, Reshotko, E., Siddiqui,^* F., Bowersox, R., “Transition Due to Roughness on Blunt Capsule: Comparison with Transient Growth Correlation,” AIAA Journal Spacecraft and Rockets Vol. 55, No. 1, pp. 167-180, 2018.
66. Radespiel, R., Ali, S., Bowersox, R., Leidy,^*, Tanno, H., Kirk, L., Reshotko, E., “Experimental Investigations of Roughness Effects on Transition on Blunt Spherical Capsule Shapes,” AIAA-2018-0059, AIAA SCITECH, Jan. 2018.
67. Corke, T., Arndt, A., Matlis, E., Neel,^*, Bowersox, R., “Hypersonic Boundary Layer Cross Flow Transition Characteristics and Control,” AIAA-2018-0352, AIAA SCITECH, Jan. 2018.
68. Neel,^*, Leidy,^* A., Tichenor, N., Bowersox, R., “Influence of Environmental Disturbances on Hypersonic Crossflow Instability on the HIFiRE-5 Elliptic Cone,” AIAA-2018-1821, AIAA SCITECH, Jan. 2018.
69. Semper,^*, Bowersox, R., “Tripping a Hypersonic Low Reynolds Number Boundary Layer,” AIAA Journal, Vol. 55, No. 3, pp. 808-817, 2017.
70. Kimmel, R., Borg, M. Jewell, J., Lam, K., Bowersox, R., and Srinivasan, R., “AFRL Ludwieg Tube Initial Performance,” AIAA SCITECH, AIAA-2017-0102, Jan. 2017.
71. Neel,^*, Leidy,^* A., and Bowersox, R., “Preliminary Study of the Effect of Environmental Disturbances on Hypersonic Crossflow Instability on the HIFiRE 5 Elliptic Cone,” AIAA SCITECH, AIAA 2017-0767, Jan. 2017.
72. Leidy,^*, Neel,^* I., Bowersox, R., and Schmisseur, J., “Influence of Perturbations on 3-D Hypersonic Shock/Laminar Boundary Interactions,” AIAA SCITECH, AIAA 2017-1685, Jan. 2017.
73. Tichenor, N., Neel,^*, Leidy,^* A., and Bowersox, R., “Influence of Streamline Adverse Pressure Gradients on the Structure of a Mach 5 Turbulent Boundary Layer,” AIAA SCITECH, AIAA 2017-1697, Jan. 2017.
74. Peltier,^*, Humble, R., and Bowersox, R., “Crosshatch Roughness Distortions on a Mach 5 Turbulent Boundary Layer,” Physics of Fluids, Vol. 28, 045105, 2016.
75. West, N., Winner, J., Bowersox, R., North, S., “Resolving the energy and temperature dependence of C6H6^∗ collisional relaxation via time-dependent bath temperature measurements,” Journal of Chemical Physics, Vol. 145, No. 1, pp. 014308-1-11, 2016.
76. Leidy, A.^*, Reshotko, E., Siddiqui,^*, Bowersox, R., “Characterizing the Transient Growth Mechanism on a Hypersonic Blunt Body at a High Angle of Attack”, 46th AIAA Fluid Dynamics Conference, AIAA AVIATION Forum, AIAA 2016-3951, June 2016.
77. Neel,^*, Leidy,^* A., Bowersox, R., Tichenor, N., “Hypersonic Boundary Layer with Streamline Curvature-Driven Adverse Pressure Gradient”, 8th AIAA Flow Control Conference, AIAA AVIATION Forum, AIAA 2016-4248, June 2016.
78. Borg, M., Kimmel, R., Hofferth, J., Mai,^*, Bowersox, R., “Freestream Effects on Boundary Layer Disturbances for HIFiRE-5,” AIAA-2015-0278, AIAA SCITECH 2015 Conference, Kissimmee, FL, Jan. 5-9, 2015. Also, AFRL Report AFRL-RQ-WP-TP-2015-0148, Wright Patterson Air Force Base, OH 2015.
79. Sánchez-González, R., McManamen,^*, Bowersox, R. and North, S.W., “A method to analyze molecular tagging velocimetry data using the Hough transform,” Review of Scientific Instruments, Vol. 86, pp. 105106-1 – 105106-14, Nov. 2015.
80. Fuller,^*J., Hsu, A., Sanchez-Gonzalez, R., Dean, J., North, S.W. and Bowersox, R., “RF-Plasma Stabilization of a Low Reynolds Number Channel Flow,” Journal of Fluid Mechanics, vol. 748, June 2014, pp. 663-691.
81. Mai,^* and Bowersox, R., “Experimental Examination of the Effect of Normal Shock Waves on Freestream Turbulence at Mach 6,” AIAA-2014-2641, AVIATION 2014 Conference, Atlanta GA, June 2014.
82. Sánchez-González, R. Bowersox, R. and North, S.W., “Vibrationally excited NO tagging by NO(A2Σ+) fluorescence and quenching for simultaneous velocimetry and thermometry in gaseous flows,” Optical Letters, 39, No. 9, 2014, pp. 2771-2774.
83. Sánchez-González, R., Eveland, W.D., Mai,^*L., Bowersox, R. and North, S.W., “Low temperature collisional quenching of NO(A²Σ⁺) (v’=0) by NO(X²∏) and O₂ between 34 and 109K,” Journal of Chemical Physics, Vol. 141, 2014, 074313.
84. Pruski,^* and Bowersox, R., “Leading Edge Flow Structure of a Dynamically Pitching 0012 Airfoil,” AIAA Journal, Vol. 51, No. 5, 2013, pp. 1042-1053.
85. Tichenor,^*, Humble, R. and Bowersox, R., “Response of Hypersonic Turbulent Boundary Layer to Favorable Pressure Gradients,” Journal of Fluid Mechanics, Vol. 722, May 2013, pp. 187-213.
86. Mendoza,^* and Bowersox, R. “On the Unsteady Shock Wave Interaction with a Backward-Facing Step: Viscous Analysis,” Paper No. 0246-000307, 29^th International Symposium on Shock Waves, Madison, WI, USA, July 14-19, 2013.
87. Mendoza,^* and Bowersox, R. “On the Unsteady Shock Wave Interaction with a Splitter Plate: Viscous Analysis,” Paper No. 0246-000324, 29^th International Symposium on Shock Waves, Madison, WI, USA, July 14-19, 2013.
88. Mendoza,^* and Bowersox, R., “On Shock-Induced Flows in 2D Ducts: Inviscid Analysis,” 51st Aerospace Sciences Meeting and New Horizons Forum and Aerospace Exposition, Grapevine, TX, Jan. 7-10, 2013.
89. Humble, R., Peltier,^*, and Bowersox, R., “Visualization of the Effects of Convex Curvature on the Outer Structure of a Hypersonic Turbulent Boundary Layer,” Physics of Fluids, Vol. 24, Oct. 2012, pp. 24-48.
90. Sánchez-González, R., Srinivasan, R., Hofferth, J., Kim, D., Tindall, A., Bowersox, R., and North, S., “Repetitively Pulsed Hypersonic Flow Apparatus for Diagnostic Development,” AIAA Journal, Vol. 50, No. 3, 2012, pp. 691-697.
91. Mendoza,^* and Bowersox, R., “On the Shock Diffraction over a 90deg. Convex Corner into a Confined Duct: Inviscid Analysis,” 20th International Shock Interaction Symposium, Stockholm, Sweden. August 20-24, 2012.
92. Mendoza,^* and Bowersox, R., “On the Unsteady Shock Wave Interaction with a Backward-Facing Step: Inviscid Analysis,” AIAA-2012-2709, 42nd AIAA Fluid Dynamics Conference, New Orleans, LA, June 25-28, 2012.
93. Taylor,^*, Mendoza,^* N. and Bowersox, R., “The Characterization and Feasibility of a Low-Duty-Cycle Fast Valve for Impulse Facilities,” AIAA-2012-2827, 42nd AIAA Fluid Dynamics Conference, New Orleans, LA, June 25-28, 2012.
94. Tichenor,^*, Humble, R., and Bowersox, R., “Reynolds Stresses in a Hypersonic Boundary Layer with Streamline Curvature-Driven Favorable Pressure Gradients,” AIAA-2012-3059, 42nd AIAA Fluid Dynamics Conference, New Orleans, LA, June 2012.
95. Peltier,^*, Humble, R., and Bowersox, R., “The Influence of Favorable Pressure Gradients upon the Coherent Motions in a Mach 5 Turbulent Boundary Layer,” AIAA-2012-3060, 42nd AIAA Fluid Dynamics Conference, New Orleans, LA, June 2012.
96. Peltier,^*, Humble, R., and Bowersox, R., “PIV of a Mach 5 Turbulent Boundary Layer over Diamond Roughness Elements,” AIAA-2012-3061, 42nd AIAA Fluid Dynamics Conference, New Orleans, LA, June 2012.
97. Sánchez-González, R. Srinivasan, R., Hofferth, J., Doyong K., Bowersox, R., North, S., “Repetitively Pulsed Hypersonic Flow Apparatus for Advanced Laser Diagnostic Development,” AIAA-2012-0733, 50^th AIAA Aerospace Sciences Meeting, Nashville, TN, Jan. 9-12, 2012.
98. Semper,^*, Pruski,^* B. and Bowersox, R., “Freestream Turbulence Measurements in a Continuously Variable Hypersonic Wind Tunnel,” AIAA-2012-0732, 50^th AIAA Aerospace Sciences Meeting, Nashville, TN, Jan. 9-12, 2012.
99. Schetz, J. and Bowersox, R., Boundary Layer Analysis, 2^nd, AIAA Ed. Series, 2011.
100. Sánchez-González, R., Srinivasan, R., Bowersox, R. and North, S., “Simultaneous Velocity and Temperature measurements in Gaseous Flow Fields using the VENOM Technique,” Optics Letters, Vol. 36, No. 2, Jan. 15, 2011.
101. Humble, R., Peltier^*, S., Lynch, K., Thurow, B., and Bowersox, R., “Visualization of Hypersonic Turbulent Boundary Layers Negotiating Convex Curvature, AIAA-2011-3419, 41st AIAA Fluid Dynamics Conference and Exhibit, Honolulu, Hawaii, June 27-30, 2011.
102. Pruski,^*, Humble, R., Bowersox, R., “Leading Edge Flow Structure of a Dynamically Pithcing 0012 Airfoil,” AIAA-2011-3257 41^st AIAA Fluid Dynamics Conference, Honolulu, Hawaii, June 27-30, 2011.
103. Saric W., Reed, H., Bowersox, R., and North, S., “Hypersonic Laminar-Turbulent Transition Studies,” 7th Aerothermodynamics Symposium, May 9-11, 2011, Brugge, Belgium.
104. Bowersox, R., “High-Speed Turbulent Boundary Layers with Roughness and Global Distortions (Invited),” 49^th Aerospace Science Meeting, Orlando, FL, Jan. 4-7, 2011.
105. Tichenor,^*, Humble, R., and Bowersox, R., “Influence of Favorable Pressure Gradients on a Mach 5.0 Turbulent Boundary Layer,” AIAA-2011-0748, 49^th Aerospace Sciences Meeting, Orlando, FL, Jan. 4-7, 2011.
106. Peltier,^*, Humble, R., and Bowersox, R., “Response of a Hypersonic Turbulent Boundary Layer to Local and Global Mechanical Distortions,” AIAA-2011-0680, 49^th Aerospace Sciences Meeting, Orlando, FL, Jan. 4-7, 2011.
107. Schneider, S. and Bowersox, R., “Hypersonic Transition and Turbulence,” Encyclopedia of Aerospace Engineering, , R. Blockley and W. Shyy, John Wiley & Sons, 2010.
108. Kobayashi, K., Bowersox, R., Srinivasan, R., Tichenor^*, N., Carter, C. and Ryan, M. “Experimental and Numerical Studies of Diamond-Shaped Injector in a Supersonic Flow,” Journal of Propulsion and Power, Vol. 26, No. 2, 2010, pp. 373-376.
109. Bowersox, R. and North, S., “Algebraic turbulent energy flux models for hypersonic shear flows,” Progress in Aerospace Sciences, 46, 2010, pp. 49-61.
110. Bowersox, R., “Modeling High-Speed Shear Flows with Non-Equilibrium Effects (A Work In-Progress), Invited Lecture, Caltech, 2010.
111. Peltier,^*, and Bowersox, R., “Periodic Surface Roughness in High-Speed Turbulent Flow,” AIAA-2010-5020, 40th Fluid Dynamics Conference, Chicago, Illinois, June 28-1, 2010.
112. Hofferth, J., Bowersox, R. and Saric, W., “The Mach 6 Quiet Tunnel at Texas A&M: Quiet Flow Performance,” AIAA-2010-4794, 27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Chicago, Illinois, June 28-1, 2010.
113. Tichenor,^* Semper,^* M., Srinivasan, R. Bowersox, R. and North, S., “Calibration of an Actively Controlled Expansion Hypersonic Wind Tunnel,” AIAA-2010-4793, 27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Chicago, Illinois, June 28-1, 2010.
114. Sánchez-González, R., Tindall, A., Bowersox, R., North, S., and Hsu, A., “Towards Simultaneous Velocimetry and Thermometry Measurements Using the VENOM Diagnostic Technique,” AIAA-2010-4349, 27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Chicago, Illinois, June 28-1, 2010.
115. Srinivasan, R., Kobayashi, K., Carter, C., and Bowersox, R., “Studies of Diamond-Shaped Injectors in a Supersonic Flow (Invited Presentation),” AIAA-2010-0379, Presented by Bowersox, 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, Florida, Jan. 4-7, 2010.
116. Hsu, A., Srinivasan, R., Bowersox, R. and North, S., “Application of Molecular Tagging Towards Simultaneous Vibrational Temperature and Velocity Mapping in an Underexpanded Jet Flowfield “, AIAA Journal, 47, No. 11, 2009, pp. 2597-2604.
117. Hsu, A., Srinivasan, R., Bowersox, R. and North, S., “Two-Component Molecular Tagging Velocimetry Utilizing NO Fluorescence Lifetime and NO2 Photodissociation Techniques in an Underexpanded Jet Flowfield,” Applied Optics, 48, Issue 22, 2009, pp. 4414–4423.
118. Bowersox, R., “Extension of Equilibrium Turbulent Heat Flux models to High-Speed Shear Flows,” Journal of Fluid Mechanics, Vol. 633, August 2009, pp. 61-70.
119. Ekoto^*, I., Bowersox, R., Beutner, T. and Goss, L., “Response of Supersonic Turbulent Boundary Layers to Local and Global Mechanical Distortions,” Journal of Fluid Mechanics, Vol. 630, July 2009, pp. 225-265.
120. Bowersox, R., “Algebraic turbulent energy flux models for hypersonic shear flows: Invited presentation,” AIAA-2009-3724, AIAA 39^th Fluid Dynamics Conference, San Antonio, TX, June 22-25, 2009.
121. Hsu, A., Srinivasan^*, R., Bowersox, R. and North, S., “Two-Component Molecular Tagging Velocimetry Utilizing NO Fluorescence Lifetime and NO2 Photodissociation Techniques in an Underexpanded Jet Flowfield,” AIAA-2009-4049, AIAA 39^th Fluid Dynamics Conference, San Antonio, TX, June 22-25, 2009.
122. Semper^*, M., Tichenor^*, N. Bowersox, R., Srinivasan, R. and North, S., “On the Design and Calibration of an Actively Controlled Expansion Hypersonic Wind Tunnel,” AIAA-2009-799, 47th AIAA Aerospace Sciences Meeting, Orlando, FL, Jan. 5-8, 2009.
123. Sahoo^*, D., Srinivasan,^* and Bowersox, R., “Examination of the Leading Edge Flow Structure of a Dynamically Pitching NACA 0012 Airfoil,” AIAA-2009-788, 47th AIAA Aerospace Sciences Meeting, Orlando, FL, Jan. 5-8, 2009.
124. Fuller^*, T., Hsu, A., Bowersox, R. and North, S., “The Effect of Vibrational Non-Equilibrium on the Decay of Grid Generated Turbulence,” AIAA-2009-593, 47th AIAA Aerospace Sciences Meeting, Orlando, FL, Jan. 5-8, 2009.
125. Hsu, A., Srinivasan^*, R., Bowersox, R. and North, S., “Application of Molecular Tagging Velocimetry Towards Simultaneous Vibrational Temperature and Velocity Mapping in an Underexpanded Jet Flowfield,” AIAA-2009-1447, 47th AIAA Aerospace Sciences Meeting, Orlando, FL, Jan. 5-8, 2009.
126. Kobayashi, K., Bowersox, R., Srinivasan^*, R., Tichenor^*, N., Carter, C. and Ryan, M., “Experimental and Numerical Studies of Diamond-Shaped Injector in a Supersonic Flow,” AIAA-2009-1420, 47th AIAA Aerospace Sciences Meeting, Orlando, FL, Jan. 5-8, 2009.
127. Srinivasan^*, R. and Bowersox, R., “Transverse Injection through Diamond and Circular Ports into a Mach 5.0 Freestream,” AIAA Journal, 46, No. 8, Aug., 2008, pp. 1944 – 1962.
128. Ekoto^*, I., Bowersox, R., Beutner, T. and Goss, L., “Supersonic Boundary Layers with Periodic Surface Roughness,” AIAA Journal, Vol. 46, No. 2, Feb., 2008, pp. 486-497.
129. Bowersox, R., North, S. and Srinivasan^*,R., “High- Speed Free Shear Layers with Molecular Non-Equilibrium: An Example of the Fluids Information Triad (Invited),” AIAA-2008-685, 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 2008.
130. Sahoo^*, D., Bowersox, R., and Goss, L., “Experimental Investigation of the Leading-Edge Flow of a Dynamically Pitching Airfoil,” AIAA-2008-651, 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 2008.
131. Kobayashi, K., Bowersox, R., Srinivasan^*, R., Carter, C. and Hsu, K., “Flow Field Studies of Diamond Shaped Fuel Injector in a Supersonic Flow,” Journal of Propulsion and Power, Vol. 23, No. 6, Nov.-Dec., 2007, pp. 1168-1176.
132. Srinivasan^*, R. and Bowersox, R., “Simulation of Transverse Gaseous Injection through a Diamond Port into a Supersonic Freestream,” Journal of Propulsion and Power, 23, No. 4, July-August 2007, pp. 772-781.
133. Kobayashi, K., Bowersox, R., Srinivasan*, R., Carter, C. and Hsu, K., “Flow Field Studies of Diamond Shaped Fuel Injector in a Supersonic Flow,” AIAA-2007-5416, 43^rd Joint Propulsion Conference, Cincinnati, OH, July 2007.
134. Bowersox, R., “High-speed Rough Wall Boundary Layers and Modeling” (invited presentation), AIAA 2007-3998, 37th AIAA Fluid Dynamics Conference, Miami FL, June 2007.
135. Ekoto^*, I., Bowersox, Beutner, T., and Goss, L., “Supersonic Turbulent Boundary Layers with Mechanical Non-Equilibrium” AIAA 2007-4561, 25th Applied Aerodynamics Conference, Miami FL, June 2007.
136. Ekoto^*, I., Bowersox, R. and Goss, L., “Planar Measurements of Supersonic Boundary Layers with Curvature Driven Pressure Gradients,” AIAA-2007-1137, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 2007.
137. Ekoto^*, I., Bowersox, Beutner, T., and Goss, L., “Response of a Supersonic Turbulent Boundary Layer to Periodic Surface Roughness,” AIAA-2007-1142, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 2007.
138. Bowersox, R. and Srinivasan^*, R., “Internal Energy Based Modeling of High-Speed Gaseous Flow Turbulence,” AIAA-2006-3534, 36^th AIAA Fluid Dynamics Conference and Exhibit, San Francisco, CA, June 5-8, 2006.
139. McLellan^*, J., Bowersox, R., and Srinivasan, R., “The Effect of Diamond Injector Geometry on Supersonic Jet Interaction Secondary Flow,” AIAA-2006-1228, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 2006.
140. Ekoto^*, I., Bowersox, R., Srinivasan*, R. and Goss, L., “Examination of Cameras for Near-Wall PIV Measurements in High-Speed flow,” AIAA-2006-0044, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 2006.
141. Mahmud^*, Z. and Bowersox, R., “Aerodynamics of Low Blowing Ratio Fuselage Injection into a Supersonic Freestream,” Journal of Spacecraft and Rockets, Vol. 42, No. 1, Jan-Feb, 2005, pp. 30-37.
142. Srinivasan^*, R. and Bowersox, R. “Comparison of RANS and DES Turbulence Models to Experiments for Supersonic TJISF,” AIAA-2005-0499, AIAA Aerospace Sci Meeting, Reno, NV, Jan. 2005.
143. Srinivasan^*, R. and Bowersox, R. “Detached-Eddy Simulation of Gaseous Injection into a Mach 5.0 Freestream,” AIAA-2005-0894, AIAA Aerospace Sci Meeting, Reno, NV, Jan. 2005.
144. Srinivasan^*, R. and Bowersox, R. “Characterization of Flow Structure and Turbulence in Hypersonic Jet Interaction Flowfields,” AIAA-2005-0895, AIAA Aerospace Sci Meeting, Reno, NV, Jan. 2005.
145. Bowersox, R., Poster Session, 2005 AFOSR Scientific Advisory Board Review, DC, 2005 (only Fluid or Gas Dynamics representative for the AFOSR at this review).
146. Byun, Y., Bae, K., Wallis, S., Viti, V., Schetz, J. and Bowersox, R., “Jet Interaction in Supersonic Flow with a Downstream Surface Ramp,” Journal of Spacecraft and Rockets, Vol. 42, No.1, Jan-Feb, 2004, pp. 38-44.
147. Viti, V., Wallis, S., Schetz, J., Neel, R., and Bowersox, R., “Jet Interaction with a Primary Jet and an Array of Smaller Jets,” AIAA Journal, Vol. 42, No. 7, July 2004, pp. 1358-1368.
148. Bowersox, R., Fan,^*, and Lee,^* D., “Sonic Injection into a Mach 5.0 Freestream through Diamond Orifices,” Journal of Propulsion and Power, Vol. 20, No. 2, 2004, pp. 280-287.
149. Srinivasan^*, R. and Bowersox, R. “High-Speed Transverse Injection Flow Tailoring via Barrel-Shock Manipulation,” AIAA-2004-2698, AIAA Flow Control Conference, Portland, OR, July 2004.
150. Marconi, F., Bowersox, R. and Schetz, J. “Sonic Boom Alleviation Using Keel Configurations,” Journal of Aircraft, Vol. 40, No. 2, 2003, pp. 363-369.
151. Karr, C.L., Bowersox, R., Singh, V., “Minimization of Sonic Boom on Supersonic Aircraft Using an Evolutionary Algorithm,” Genetic and Evolutionary Computation — GECCO 2003 Lecture Notes in Computer Science, 2724, 2003, pp. 2157-2167
152. Bowersox, R., Fan^*, H., and Lee^*, D., “Sonic Injection into a Mach 5.0 Freestream through Diamond Shaped Orifices at Various Incidence,” AIAA-2003-5190, AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Huntsville, AL, July 2003.
153. Srinivasan^*, R. and Bowersox, R., “Numerical Analyses of Gaseous Injection into a Mach 5.0 Freestream through Diamond Orifices,” AIAA-2003-5188, AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Huntsville, AL, July 2003.
154. Byun, Y., Wallis, S., Viti, V., Bae, K., Schetz, J. and Bowersox, R., “Jet Interaction in Supersonic Flow with a Surface Ramp,” AIAA 2003-3933, June 2003.
155. Mahmud^*, Z. and Bowersox, R., “Supersonic Missile Body Jet Interaction Flowfields at Low Momentum-Ratio-Parameter,” 41^st AIAA Aerospace Sci Meeting, Reno NV, Jan 2003.
156. Wilson, E., Bowersox, R. and Karr, C., “Minimization of Sonic Boom with Genetic Algorithms,” 41^st AIAA Aerospace Sciences Meeting, Reno NV, Jan 2003.
157. Latin^*, R. and Bowersox, R., “Temporal Turbulent Flow Structure for Supersonic Rough-Wall Boundary Layers,” AIAA Journal, 40, No. 5, 2002, pp. 832-841.
158. Wallis, S. and Schetz, J. and Bowersox, R., “Jet Interaction with a Main Jet and an Array of Smaller Jets: Part A – Experimental Studies,” AIAA Paper 2002-3148, 20th AIAA Applied Aerodynamics Conference, St. Louis, MO, June 2002.
159. Marconi, F., Bowersox, R., Orr, M., Mozingo, J. and Schetz, J., “Sonic Boom Alleviation Using Keel Configurations,” AIAA-2002-0149, 40^th Aerospace Science Meeting, Reno NV, Jan. 2002.
160. Fan^*, H. and Bowersox, “Gaseous Injection through Diamond Orifices at Various Incidence Angles into a Hypersonic Freestream,” AIAA 2001-1050, 39^th AIAA Aerospace Sciences Meeting, Reno NV, Jan 2001.
161. Pritchett^*, V. and Bowersox, “Flow Properties of Compressible and Incompressible Subsonic Turbulent Boundary Layers with Surface Roughness,” AIAA Paper 2001-1021, 39^th AIAA Aerospace Sciences Meeting, Reno NV, Jan 2001.
162. Mahmud^*, Z., and Bowersox, R., “Experimental Investigation of Low Blowing Ratio Blended Body Supersonic Injection Flowfields,” AIAA Paper 2001-0886, 39^th AIAA Aerospace Sciences Meeting, Reno NV, Jan 2001.
163. Latin^*, R. and Bowersox, R., “Flow Properties of a Supersonic Boundary Layer with Wall Roughness,” AIAA Journal, 38, No. 10, 2000, pp. 1804-1821.
164. Luker^*, J., Bowersox, R., and Buter, T., “Influence of A Curvature Driven Favorable Pressure Gradient on a Supersonic Turbulent Boundary Layer,” AIAA Journal, 38, No. 8, 2000, pp. 1351-1359.
165. Bowersox, R., Tucker^*, K., and Whitcomb^*, C., “Two-Dimensional Nonadiabatic Injection into a Supersonic Freestream,” Journal of Propulsion and Power, March-April, 2000, pp. 234-242.
166. Bowersox, R., Wier^*, R., Glawe, D., and Gogineni, S., “Measurements of Turbulent Flow Structure in Supersonic Curved Wall Boundary Layers,” Journal of Propulsion and Power, 16, No. 1, 2000, pp. 153-154.
167. Bowersox, R., “Uncertainty Analysis of the Mach 6.0 Hyper-X Free Flyer and Booster Separation Wind Tunnel Data,” Hyper-X Program Office HX-703, SSD-00-07, Nov. 2000.
168. Chenault^*, L., Beran, P., and Bowersox, R., “Second-Order Reynolds Stress Turbulence Modeling of Three-Dimensional Oblique Supersonic Injection,” AIAA Journal, 37, No. 10, 1999, pp. 1257-1269.
169. Wilson^*, M., Bowersox, R., and Glawe, D., “An Experimental Investigation of the Role of Downstream Ramps on a Supersonic Injection Plume,” Journal of Propulsion and Power, 15, No. 3, 1999, pp. 432-439.
170. Latin^*, R. and Bowersox, R., “Influence of Surface Roughness on Supersonic Boundary Layer Turbulent Flow Structure,” 14^th International Symposium on Airbreathing Engines (XIV ISABE), Florence, Italy, Sept. 5-10, 1999.
171. Chenault^*, C., Beran, P., and Bowersox, R., “Numerical Investigation of 3D Oblique Supersonic Injection Using a Second-Order Reynolds Stress Turbulence Model,” 14^th International Symposium on Airbreathing Engines (XIV ISABE), Florence, Italy, Sept. 5-10, 1999.
172. Fan^*, H. and Bowersox, “Numerical Analysis of High-Speed Flow Over Rough Surfaces,” AIAA-99-2381, 35^thAIAA/ASME/SAE/ASEE Joint Propulsion Conference, Los Angeles CA, June 1999.
173. Payne, M., Bowersox, R., Chrissis, J., Pohl, E., Gruber, M., and Fuller, R., “A Variable-Complexity Modeling Approach to Scramjet Fuel Injection Array Design Optimization,” AIAA-99-2251, 35^th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Los Angeles CA, June 1999.
174. Latin^*, R. and Bowersox, R., “Influence of Surface Roughness on the Mean and Turbulent Flow Properties of Supersonic Boundary Layer,” AIAA-99-1017, AIAA 37^th Aerospace Sciences Meeting, Reno, NV, Jan. 1999.
175. Tilmann^*, C., and Bowersox, R., “On the Design and Construction of an Academic Mach 4.9 Wind Tunnel,” AIAA-99-0800, AIAA 37^th Aerospace Sciences Meeting, Reno, NV, Jan. 11-14, 1999.
176. Gogineni, S. and Bowersox, R., “Flow Control Methods for Hypersonic Flows”, APS Centennial Meeting, Atlanta, GA, March 23-26, 1999.
177. Gogineni, S., Bowersox, R. and Hinke, M., “Control of Vortex Asymmetry using Microjet Blowing in Hypersonic Flows,” 24th Annual Dayton-Cincinnati Aerospace Science Symposium, Dayton, OH April 9, 1999.
178. McIntyre^*, T., Bowersox, R., and Goss, L., “Experimental Investigation of Supersonic Wrap-Around Fin Aerodynamic Mach Number Effects,” Journal of Spacecraft and Rockets, 35, No. 6, 1998, pp. 742-748.
179. Tilmann^*, C., Buter, T., and Bowersox, R., “Characterization of the Flowfield near a Wrap-Around Fin at Mach 2.8,” Journal of Aircraft, 35, No. 6, 1998, pp. 868-875.
180. Luker^*, J., Hale^*, C., and Bowersox, R., “Experimental Characterization of the Turbulent Shear Stresses for Distorted Supersonic Boundary Layers,” Journal of Propulsion and Power, 14, No. 1, 1998, pp. 110-118.
181. Tilmann^*, C., McIntyre^*, T., Bowersox, R., and Buter, T., “Aerodynamics of Wrap-Around Fins at High Supersonic Speeds,” RTO-AVT Panel on Missile Aerodynamics, May 11-15, 1998 Sorrento Italy.
182. Tilmann^*, C., Bowersox, R. and Buter, T., “Characterization of the Flowfield Near A Wrap-Around Fin at Mach 4.9,” in the proceedings of The Technical Cooperation Program Meeting, WPN Group Technical Panel, W-2, Bedford UK, April 27 – May 1, 1998.
183. Latin*, R. and Bowersox, R., “The Influence of Surface Roughness on Supersonic High Reynolds Number Turbulent Boundary Layer Flow,” AFRL-PR-WP-TR-1999-2004, Propulsion Directorate, Air Force Research Laboratory, Air Force Material Command, Wright-Patterson AFB, OH March 1998.
184. Tucker^*, K., Whitcomb^*, C., and Bowersox, R., “Turbulence and Meanflow Measurements Downstream of a Two-Dimensional Supersonic Normal Injection into a Supersonic Freestream,” AIAA-98-3274, 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cleveland OH, July 13-15, 1998.
185. Hazelton^*, D. and Bowersox, R., “Skin Friction Correlations for High Enthalpy Flows,” AIAA-98-1636, AIAA 8th International Space Planes and Hypersonic Systems and Technologies Conference, Norfolk, VA, April 27-30, 1998.
186. Wier^*, R., Bowersox, R., Glawe, D., and Gogineni, S., “Structure of a Compressible Boundary Layer over a Curved Wall,” AIAA-98-0621, AIAA 36th Aerospace Sciences Conference, Reno NV, Jan. 6-9, 1998.
187. Tilmann^*, C. and Bowersox, R., “Characterization of the Flowfield Near A Wrap-Around Fin At Mach 4.9,” AIAA-98-0684, AIAA 36th Aerospace Sciences Conference, Reno NV, Jan. 6-9, 1998.
188. Tilmann^*, C., Huffman, R., Buter, T., and Bowersox, R., “Experimental Investigation of the Flow Structure near a Wrap-Around Fin at Supersonic Speeds,” Journal of Spacecraft and Rockets, 34, No. 6, 1997, pp. 729-735.
189. Gardner, P., Roggemann, M., Welsh, B., Bowersox, R., and Luke, T., “Comparison of Measured and Computed Strehl Ratios for Light Propagation through a Channel Flow of a He-N₂ Mixing Layer at High Reynolds Numbers,” Applied Optics, Vol. 36, No. 12, 1997, pp. 2559-2567.
190. Hazelton^*, D., Bowersox, R., and Schetz, J., “Skin Friction Measurements in Scramjet Tests,” ISABE 97-7065, Proceedings of the 1997 JANNAF Airbreathing Propulsion Subcommittee Annual Meeting, CPIA, Palm Beach, FL, Oct. 1997 (Restricted).
191. Hazelton^*, D., and Bowersox, R., “Analysis of Beam Geometry and Viscous Oil Damping for Improved High Frequency Skin Friction Gauge,” in Papers from the Thirteenth International Symposium on Airbreathing Engines, Proceedings of the XIII International Symposium on Air Breathing Engines, Air Breathing Challenges of the 21st Century, Sept. 8-12, 1997, Vol. 1, pp. 448-456.
192. Gogineni, S., Goss, L., Glawe, D., Bowersox, R., and Wier^*, R., “Digital Two-Color PIV and Flow Visualization Studies for Complex Supersonic Flows,” Proceedings of the ASME Fluids Engineering Division Summer Meeting on Experimental and Numerical Flow Visualization and Laser Anemometry, FEDSM97-3092 (on CD), Vancouver, British Columbia, Canada, June 22-26, 1997.
193. McIntyre^*, T., Bowersox, R., Goss, L. and Trump, D., “Loading Analysis of Wrap-Around Fin Missile Aerodynamics Using Pressure Sensitive Paint,” 17 Int Congress on Instrumentation in Aerospace Simulation Facilities (ICIASF), Monterey CA, Sept. 29-Oct. 2, 1997.
194. Wilson^*, M., Bowersox, R., and Glawe, D., “Role of Downstream Ramps on Penetration and Mixing for Supersonic Injection Flows,” AIAA-97-2887, 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Seattle WA, July 6-9, 1997.
195. Hazelton^*, D., Bowersox, R., Nuemann, D., and Hayes, J., “Skin Friction Measurements in a Mach 6 Inlet Test,” AIAA-97-2884, 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Seattle WA, July 6-9, 1997.
196. Davis^*, D., and Bowersox, R., “Perfectly Stirred Reactor Analysis of SCRAMjet Cavity Flame Holders,” AIAA-97-3274, 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Seattle WA, July 6-9, 1997.
197. Davis^*, D., and Bowersox, R., “CFD Analysis of SCRAMjet Cavity Flame Holders,” AIAA-97-3270, 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Seattle WA, July 6-9, 1997.
198. Novean, M. Schetz, J., and Bowersox, R., “Direct Measurement of Skin Friction in Complex Supersonic Flows,” AIAA 97-0394, AIAA 35th Aerospace Sciences Conference, Reno NV, Jan. 6-9, 1997.
199. Luker^*, J., Hale^*, C., and Bowersox, R., “Experimental Analysis of the Turbulent Shear Stresses for Distorted Supersonic Boundary Layers,” AIAA 97-0426, AIAA 35th Aerospace Sciences Meeting, Reno, NV, Jan. 6-9, 1997.
200. Meyer, M., Buter, T., and Bowersox, R., “Turbulence Measurements in a Supersonic Boundary Layer with Impinging Shock Wave Interaction,” AIAA 97-0427, AIAA 35th Aerospace Sciences Conference, Reno NV, Jan. 6-9, 1997.
201. Bowersox, R., “Thermal Anemometry,” Handbook of Fluid Dynamics & Fluid Machinery, John Wiley & Sons, Sect. 15.4.2, 1996, pp. 965-983.
202. Bowersox, R. “Refractive Optical Flow Visualization Techniques,” Handbook of Fluid Dynamics & Fluid Machinery, John Wiley & Sons, Sect. 15.6.2, 1996, pp. 1022-1039.
203. Bowersox, R., “Combined Laser Doppler Velocimetry and Cross-Wire Anemometry Analysis for Supersonic Turbulent Flow,” AIAA Journal, 34, No. 11, 1996, pp. 2269-2275.
204. Bowersox, R., and Buter, T., “Mass-Weighted Turbulence Measurements in a Mach 2.9 Boundary Layer with Mild Adverse and Favorable Pressure Gradient,” AIAA Journal, Vol. 34, No. 12, 1996, pp. 2470-2483.
205. Bowersox, R., “Turbulent Flow Structure Characterization of Angled Injection in a Supersonic Cross Flow,” Journal of Spacecraft and Rockets, Vol. 34, No. 2, 1996, pp. 205-313.
206. Gardner, P., Roggemann, M., Welsh, B., Bowersox, R., and Luke, T., “Statistical Anisotropy in Free Turbulence for Mixing Layers at High Reynolds Numbers,” Applied Optics, Vol. 35, No. 24, 1996, pp. 4879-4889.
207. Chen, F., Bowman, J., and Bowersox, R., “Effects of Transpiration Cooling on Nozzle Heat Transfer,” Journal of Spacecraft and Rockets, Vol. 33, No. 3, 1996, pp. 453-455.
208. Roggemann, M., Gardner, P., Welsh, B., Bowersox, R., and Jewell, D., “Gas Flow Visualization by Means of Sheared Beam Interferometry: Sensitivity, Dynamic Range, and Integrated Density Estimation,” Measurement, Vol. 17, No. 4, 1996, pp. 251-265.
209. Senseney, M., Buter, T., and Bowersox, R., “Flow Structure and Performance Characterization of a Highly-Offset Diffuser with and Without Vortex Generator Jets,” Journal of Propulsion and Power, 12, No. 2, 1996, pp. 237-244.
210. McCann^*, G., and Bowersox, R., “Measurements across the Plume of a Low-Angled Supersonic Gaseous Injection into a Supersonic Free Stream,” AIAA Journal, 34, No. 2, 1996, pp. 317-323.
211. Tilmann^*, C., Huffman. R., Buter, T., Bowersox, R., “Characterization of the Flow Structure in the Vicinity of a Wrap-Around Fin at Supersonic Speeds,” AIAA-96-0190, AIAA 34th Aerospace Sciences Meeting, Reno, NV, 1996.
212. Hazelton^*, D., Bowersox, R. and Schetz, J., “Directional Skin Friction Measurements in a High Enthalpy Supersonic Flow about a Sharp Fin,” AIAA-96-4503, AIAA 7th International Space Planes and Hypersonic Systems and Technologies Conference, Norfolk, VA, Nov. 18-22, 1996.
213. Huffman, R., Tilmann^*, C., Buter, T., and Bowersox, R., “Experimental Investigation of the Flow Structure in the Vicinity of a Single Wrap-Around Fin at Mach 2.9,” AIAA-96-2450, AIAA 14th Applied Aerodynamics Conference, New Orleans, LA, June, 17-20, 1996.
214. Novean, M., Schetz, J., and Bowersox, R., “Direct Measurements of Skin Friction in Complex Supersonic Flows,” VPI-AOE-231 (Final report NASA Grants CA-NCC2-5040 and NAS1-19610-21), April, 1996, 150 pages.
215. Glawe, D., Bowersox, R., Goss, L., Terry, W., Dasgupta, S., and Gogineni, S., “Digital Two-Color PIV Measurements in a Mach-2.8 Boundary Layer,” AIAA-96-2799, 32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Lake Buena Vista, FL, July 1-3, 1996.
216. Dasgupta, S., Terry, W., Vuppuladhadium, R., Bowersox, R., Glawe, D., and Nejad, A., “A Two-Color Particle Imaging Velocimetry System for Supersonic Flow Studies,” AIAA-96-2798, 32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Lake Buena Vista, FL, July 1-3, 1996.
217. Weir^*, R., Bowersox, R., Glawe, D., Gogineni, S., and Goss, L., “Experimental Investigation of Distorted Supersonic Turbulent Boundary Layers,” presented at the 49th Annual Meeting of the APS Division of Fluid Dynamics, Syracuse, NY, 24-26 Nov. 1996.
218. Glawe, D., R. Bowersox, R., Gogineni, S., and Goss, L., “Development of High-Resolution Digital Two-Color PIV (D2CPIV) for Supersonic Turbulent Flows,” presented at the 49th Annual Meeting of the APS Division of Fluid Dynamics, Syracuse, NY, 24-26 Nov. 1996.
219. Keener^*, D., Lenertz, J., Bowersox, R., and Bowman, J., “Transpiration Cooling Effects on Nozzle Heat Transfer and Performance,” Journal of Spacecraft and Rockets, Vol. 32, No. 6, 1995, pp. 981-985.
220. Bowersox, R. and Schetz, J., “Measurements of Compressible Flow Structure in a Supersonic Mixing Layer,” AIAA Journal, Vol. 33, No. 11, 1995, pp. 2101-2106.
221. Bowersox, R., Schetz, J., and Conners, R., “Digital Analysis of Shadowgraph Images for Statistical Index of Refraction (Density) Turbulent Fluctuation Properties in High-Speed Flow,” Measurement, Vol. 15, No. 3, 1995, pp. 201-209.
222. Bowersox, R., Schetz, J., Chadwick, K., and Deiwert, S., “A Technique for Direct Measurement of Skin Friction in High Enthalpy Impulsive SCRAMjet Flow Fields,” AIAA Journal, Vol. 33, No. 7, 1995, pp. 1286-1291.
223. Miller, R., Dotter*, J., Bowersox, R., and Buter, T., “Measurements of Compressible Turbulence in a Supersonic Wall Bounded Flow with Pressure Gradient,” 2nd Symposium on Transitional and Turbulent Compressible Flows, Joint ASME/JSME Fluids Engineering Conference, Hilton Head SC, FED-Vol. 224, 1995, pp. 193-200.
224. Bowersox, R.D.W. and Schetz, J.A., “Measurements of Mean Flow and Favre-Averaged Fluctuation Properties in a Supersonic High Reynolds Number Turbulent Mixing Layer,” Fourth Pan-American Congress on Applied Mechanics, L. Godoy, S. Idelsohn, P. Laura and D. Mook (Eds.), Amer. Acad. Mech., Jan. 1995.
225. Davis^*, D., and Bowersox, R., “Numerical Analysis of Recessed Flame Holders for SCRAMjet Applications,” 1995 JANNAF, 32nd Combustion Subcommittee Meeting, NASA Marshall Space Flight Center, Huntsville, AL, Oct. 1995 (restricted).
226. Novean, M., Schetz, J., Hazelton^*, D., and Bowersox, R., “Skin Friction Measurements in Short Duration High Enthalpy Flows,” AIAA-95-6109, AIAA/DLGR/JSASS/RAeS 6th International Aerospace Planes and Hypersonics Technologies Conference, Chattanooga, TN, April 3-5, 1995.
227. Gardner, P., Roggemann, M., Welsh, B., and Bowersox, R., “Statistical Assessment of Optical Phase Fluctuations through Turbulent Mixing Layers,” SPIE Proceedings: Optical Techniques in Fluid, Thermal, and Combustion Flows,” SPIE 1995 International Symposium on Optical Science, Engineering and Instrumentation, San Diego, CA, July 1995 (Paper number 2546-26).
228. Bowersox, R. and Schetz, J., “A Model for Compressible Turbulence in Hypersonic Wall Boundary and High-Speed Mixing Layers,” AIAA Journal, Vol. 32, No. 7, 1994, pp. 1531-1533.
229. Bowersox, R. and Schetz, J., “Compressible Turbulence Measurements in a High-Speed High
230. Bowersox, R. and Schetz, J., “Compressible Turbulence Measurements in a High-Speed High Reynolds Number Mixing Layer,” AIAA-94-0819, 32^st Aerospace Sciences Meeting, Reno NV, Jan. 1994.
231. Bowersox, R. and Schetz, J., “Skin Friction Gauges for High Enthalpy Impulsive Flows,” AIAA-93-5079, AIAA/DGLR 5th International Aerospace Planes and Hypersonics Conference, Munich Germany, 1993.
232. Bowersox, R. and Schetz, J., “A Model for Compressible Turbulence in Hypersonic Wall Boundary and High-Speed Mixing Layers,” AIAA-93-0660, 31^st Aerospace Sciences Meeting, Reno NV, Jan. 1993.
233. Bowersox, R., Ng, W., and Schetz, J., “Hot-Wire Techniques Evaluated in the Wake of a 2-D Supersonic Compressor Cascade,” Yokohama IGTC-84, 1991, pp. 303-309.

Invited Lectures/Presentations and Panel Discussions (Bowersox)

1. Participant, AFOSR/ONR/NASA HTP Joint Boundary Layer Transition Workshop, June 2023.
2. Invited Speaker (Virtual), WPN Weapon Launch and Flight Dynamics, TP-5 Weapons Flight Sciences, Ottawa, Canada, April 2023.
3. Panel Member, Advancement in Computational Simulation for Design, Analysis, and Virtual Flight Test, Hypersonic Weapon Systems Summit, Arlington VA, April 2023.
4. Panel Member, Leveraging UCAH to Help Advance DoD Requirements in Hypersonics-related S&T, Workforce Development, and Technology Transition, Navy 2^nd Annual Hypersonics Innovation Conference, Dayton, OH, May 2023.
5. Dryden Award Lecture, “Hypersonic Viscous Flow: Theory, Ground Test, and Flight,” AIAA SCITECH, Jan. 2023.
6. Raytheon AIAA Tucson Mini Seminar Series, “Hypersonic Boundary Layer Turbulence (BOLT-II) In Memory of Mike Holden Flight Experiment,” Nov. 2022
7. Panel Member, AIAA Technical Panel: High-Speed Ground Test: Challenges and Opportunities for the Next Generation, AIAA AVIATION Forum, June 2022.
8. Panel Member, AIAA Panel: Recent Advances in High-Speed Flight Test, HSABP-05, AIAA AVIATION Forum, June 2022.
9. Panel Member, Innovation Speed and Overcoming Speedbumps, NDIA, Virtual, Dec. 2021,
10. University of Michigan, “Hypersonic Turbulence Boundary Layers,” Virtual, Nov. 2021.
11. Hypersonic Defense, “Supporting Hypersonic Flight Through UCAH and Research,” Arlington, VA, Nov. 2021.
12. HTSC Webinar, “TAMU Aerothermochemistry and Hypersonics Laboratory,” Virtual, Oct. 2021.
13. Raytheon RTX Technical Fellows Seminar, “Supporting Hypersonic Flight Through UCAH and Research,” Virtual, Oct. 2021.
14. Military Hypersonic Weapon Systems Webinar, “TAMU Aerothermochemistry and Hypersonics Laboratory,” Virtual, Oct. 2021.
15. AIAA HyTASP Webinar, “Supporting Hypersonic Flight Through UCAH and Research,” Sept. 20, 2021.
16. Panel Member, University Hypersonics Panel, NDIA Hypersonics Summit 2.0, Purdue, IN, Aug. 2021.
17. Panel Member, Virtual, Technologies and Processes for Future Aviation Systems, AIAA AVIATION, Aug. 2021.
18. Panel Member, Generating a US Hypersonics Workforce, Defense Strategies Institute DoD Hypersonics Capabilities Symposium, Oxen Hill, MD, July 2021.
19. Panel Moderator, Accelerating Hypersonics Development, AAS John Glenn Symposium, Virtual, July 2021.
20. Invited Speaker NDIA-JADC2 Conference, “Hypersonics Aerothermochemistry at TAMU,” College Station, TX, July 2021.
21. Panel Member, HSTC Wind Tunnel & Aerothermal Test Capabilities Seminar, Virtual, July 2021.
22. Plenary Speaker, OUSD (R&E) JHTO Hypersonic Reacting and Non-Reacting Turbulence Workshop, Virtual, May 2021.
23. Panel Lead, Experimental Methods in Hypersonic Turbulence, OUSD (R&E) JHTO Hypersonic Reacting and Non-Reacting Turbulence Workshop, Virtual, May 2021.
24. Panel Member, External Flows / Aerothermochemistry, OUSD (R&E) JHTO Hypersonic Reacting and Non-Reacting Turbulence Workshop, Virtual, May 2021.
25. Invited Speaker, Experimental Aerothermodynamics Research for Hypersonics, OUSD (R&E) JHTO Virtual Workshop on New Scientific Question for Basic Research, April-May 2021.
26. Panel Member, IDGA Hypersonic Weapons Summit, Virtual, April 2021.
27. Virginia Tech, “Hypersonic Viscous Flows,” Virtual, Feb. 2021.
28. Panel Member, IDGA Hypersonic Weapons Summit, Virtual, Oct. 2020.
29. Hypersonics Panel, 2019 AAS John Glenn Memorial Symposium, July 2019.
30. DoD Basic Research Forum, “Turbulence Transport in Non-Equilibrium Environments,” Arlington, VA, August 2018.
31. Panel Discussion on Hypersonics, AIAA Propulsion and Energy Forum Conf., 360, July 2018.
32. University of Illinois at Urban Champaign, “Experimental Studies on Hypersonic Transitional Flows,” April 2018.
33. University of Minnesota, “Hypersonic Turbulent Boundary Layer Flows,” March 30, 2018.
34. Purdue University, “Hypersonic Aerothermochemical Research,” Oct. 2017.
35. University of Washington, “Hypersonic Turbulent Boundary Layer with Mechanical Non-Equilibrium,” Nov. 2016.
36. Georgia Tech, “Role of Mechanical Non-Equilibrium on a Hypersonic Turbulent Boundary Layer,” Jan 2016.
37. Ohio State University, “Role of Crosshatch Roughness on a Hypersonic Turbulent Boundary Layer,” Sept. 2015.
38. University of Michigan, “Role of Crosshatch Roughness on a Hypersonic Turbulent Boundary Layer, A Work in Progress,” April 2015.
39. AFOSR Panel, Opportunities for Collaboration, JAXA, Japan, June 2015.
40. AFOSR Panel, Opportunities for Collaboration, UQ, Australia, June 2015.
41. AFOSR Panel, Opportunities for Collaboration, UNSW, Australia, June 2015.
42. Caltech, “Plasma Stabilization of a Low Reynolds Number Channel Flow,” 2014.
43. Fluid Structure Interaction Oral Session, “Turbulence Response to Local Pressure Gradients at Mach 5,” AVIATION 2014, Atlanta, GA, 2014.
44. University of Illinois at Urban Champaign, “High-Speed Boundary Layers with Non-Equilibrium Effects,” Oct. 2012.
45. Princeton University, “Algebraic Heat Flux Modeling in High-Speed Turbulent Flows with Thermal and Mechanical Non-Equilibrium,” Workshop on Turbulence in High-Speed Flow, May 2011.
46. Caltech, “Modeling High-Speed Shear Flows with Non-Equilibrium Effects – A Work In-Progress,” 2010.
47. Caltech, “Characterization and Control of Vorticity in High-Speed Jet Interaction Flows – A Work In-Progress,”
48. University of Texas, Austin, “Supersonic Flow Over Curved Surfaces,” 2003.