| Boundary layer analysis JA Schetz, RDW Bowersox American Institute of Aeronautics and Astronautics, 2011 | 488 | 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 | 86 | 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 | 84 | 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 | 83 | 2009 |
| 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 | 79 | 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 | 72 | 2013 |
| AFRL Ludwieg tube initial performance RL Kimmel, MP Borg, JS Jewell, KIY Lam, RD Bowersox, R Srinivasan, ... 55th AIAA Aerospace Sciences Meeting, 0102, 2017 | 66 | 2017 |
| Flow properties of a supersonic turbulent boundary layer with wall roughness RM Latin, RDW Bowersox AIAA journal 38 (10), 1804-1821, 2000 | 66 | 2000 |
| 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 | 62 | 1997 |
| 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 | 58 | 2012 |
| Leading-edge flow structure of a dynamically pitching NACA 0012 airfoil BJ Pruski, RDW Bowersox AIAA journal 51 (5), 1042-1053, 2013 | 53 | 2013 |
| Transverse injection through diamond and circular ports into a Mach 5.0 freestream R Srinivasan, RDW Bowersox AIAA journal 46 (8), 1944-1962, 2008 | 53 | 2008 |
| 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 | 53 | 2000 |
| 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 | 52 | 2010 |
| 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 | 50 | 2009 |
| Computational fluid dynamics analysis of cavity flame holders for scramjets D Davis, R Bowersox, D Davis, R Bowersox 33rd Joint Propulsion Conference and Exhibit, 3270, 1997 | 50 | 1997 |
| 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), 2012 | 48 | 2012 |
| 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 | 47 | 1995 |
| Supersonic boundary layers with periodic surface roughness IW Ekoto, RDW Bowersox, T Beutner, L Goss AIAA journal 46 (2), 486-497, 2008 | 46 | 2008 |
| Vibrationally excited NO tagging by NO(A2Σ+) fluorescence and quenching for simultaneous velocimetry and thermometry in gaseous flows R Sánchez-González, RDW Bowersox, SW North Optics letters 39 (9), 2771-2774, 2014 | 45 | 2014 |
Nathan TichenorTexas A&M UniversityDirección de correo verificada de tamu.edu
