Bowersox, Rodney
Bowersox, Rodney
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Cited by
Boundary layer analysis
JA Schetz, RDW Bowersox
American Institute of Aeronautics and Astronautics, 2011
Numerical investigation of supersonic injection using a Reynolds-stress turbulence model
CF Chenault, PS Beran, RDW Bowersox
AIAA journal 37 (10), 1257-1269, 1999
Simultaneous velocity and temperature measurements in gaseous flow fields using the VENOM technique
R Sánchez-González, R Srinivasan, RDW Bowersox, SW North
Optics letters 36 (2), 196-198, 2011
Molecular tagging using vibrationally excited nitric oxide in an underexpanded jet flowfield
AG Hsu, R Srinivasan, RDW Bowersox, SW North
AIAA journal 47 (11), 2597-2604, 2009
Stirred reactor analysis of cavity flame holders for scramjets
D Davis, R Bowersox, D Davis, R Bowersox
33rd Joint Propulsion Conference and Exhibit, 3274, 1997
Two-component molecular tagging velocimetry utilizing NO fluorescence lifetime and NO2 photodissociation techniques in an underexpanded jet flowfield
AG Hsu, R Srinivasan, RDW Bowersox, SW North
Applied Optics 48 (22), 4414-4423, 2009
Response of a hypersonic turbulent boundary layer to favourable pressure gradients
NR Tichenor, RA Humble, RDW Bowersox
Journal of Fluid Mechanics 722, 187-213, 2013
Simultaneous velocity and temperature measurements in gaseous flowfields using the vibrationally excited nitric oxide monitoring technique: a comprehensive study
R Sánchez-González, RDW Bowersox, SW North
Applied optics 51 (9), 1216-1228, 2012
Flow properties of a supersonic turbulent boundary layer with wall roughness
RM Latin, RDW Bowersox
AIAA journal 38 (10), 1804-1821, 2000
Influence of curvature-driven favorable pressure gradient on supersonic turbulent boundary layer
JJ Luker, RDW Bowersox, TA Buter
AIAA journal 38 (8), 1351-1359, 2000
Transverse injection through diamond and circular ports into a Mach 5.0 freestream
R Srinivasan, RDW Bowersox
AIAA journal 46 (8), 1944-1962, 2008
Experimental investigation of supersonic gaseous injection into a supersonic freestream
GJ McCann, RDW Bowersox
AIAA journal 34 (2), 317-323, 1996
AFRL Ludwieg tube initial performance
RL Kimmel, MP Borg, JS Jewell, KIY Lam, RD Bowersox, R Srinivasan, ...
55th AIAA Aerospace Sciences Meeting, 0102, 2017
Leading-edge flow structure of a dynamically pitching NACA 0012 airfoil
BJ Pruski, RDW Bowersox
AIAA journal 51 (5), 1042-1053, 2013
Response of supersonic turbulent boundary layers to local and global mechanical distortions
IW Ekoto, RDW Bowersox, T Beutner, L Goss
Journal of Fluid Mechanics 630, 225-265, 2009
Visualization of the structural response of a hypersonic turbulent boundary layer to convex curvature
RA Humble, SJ Peltier, RDW Bowersox
Physics of Fluids 24 (10), 106103, 2012
The Mach 6 quiet tunnel at Texas A&M: quiet flow performance
J Hofferth, R Bowersox, W Saric
27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 4794, 2010
Compressible turbulence measurements in a high-speed high-Reynolds-number mixing layer
RDW Bowersox, JA Schetz
AIAA journal 32 (4), 758-764, 1994
Supersonic boundary layers with periodic surface roughness
IW Ekoto, RDW Bowersox, T Beutner, L Goss
AIAA journal 46 (2), 486-497, 2008
Transpiration cooling effects on nozzle heat transfer and performance
D Keener, J Lenertz, R Bowersox, J Bowman
Journal of Spacecraft and Rockets 32 (6), 981-985, 1995
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