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Rodney D. W. Bowersox

Rodney D. W. Bowersox

D-Index & Metrics

Mechanical and Aerospace Engineering

D-Index
30
Citations
2794
World Ranking
3430
National Ranking
1146

Research.com Recognitions

  • 2004 - Fellow of the American Society of Mechanical Engineers

Best Publications

  • Numerical Investigation of Supersonic Injection Using a Reynolds-Stress Turbulence Model

    Clarence F. Chenault;Philip S. Beran;Rodney D. W. Bowersox

  • Simultaneous velocity and temperature measurements in gaseous flow fields using the VENOM technique.

    Rodrigo Sánchez-González;Ravi Srinivasan;Rodney D. W. Bowersox;Simon W. North

  • Molecular Tagging Using Vibrationally Excited Nitric Oxide in an Underexpanded Jet Flowfield

    Andrea G. Hsu;Ravi Srinivasan;Rodney D. W. Bowersox;Simon W. North

  • Two-component molecular tagging velocimetry utilizing NO fluorescence lifetime and NO2 photodissociation techniques in an underexpanded jet flowfield.

    Andrea G. Hsu;Ravi Srinivasan;Rodney D. W. Bowersox;Simon W. North

  • Response of a hypersonic turbulent boundary layer to favourable pressure gradients

    Unknown

  • Flow Properties of a Supersonic Turbulent Boundary Layer with Wall Roughness

    Unknown

  • Transverse Injection Through Diamond and Circular Ports into a Mach 5.0 Freestream

    Unknown

  • Experimental investigation of supersonic gaseous injection into a supersonic freestream

    Gregory J. McCann;Rodney D. W. Bowersox

  • Boundary Layer Analysis, Second Edition

    Joseph A. Schetz;Rodney D. W. Bowersox

  • Calibration of an Actively Controlled Expansion Hypersonic Wind Tunnel

    Nathan R. Tichenor;Michael T. Semper;Rodney D. W. Bowersox;Ravichandra Srinvasan

  • Supersonic Boundary Layers with Periodic Surface Roughness

    Unknown

  • AFRL Ludwieg Tube Initial Performance

    Roger L. Kimmel;Matthew P. Borg;Joseph S. Jewell;KIng-Yiu Lam

  • Simultaneous velocity and temperature measurements in gaseous flowfields using the vibrationally excited nitric oxide monitoring technique: a comprehensive study

    Rodrigo Sánchez-González;Rodney D. W. Bowersox;Simon W. North

  • Visualization of the structural response of a hypersonic turbulent boundary layer to convex curvature

    Unknown

  • Response of supersonic turbulent boundary layers to local and global mechanical distortions

    Unknown

  • Influence of Curvature-Driven Favorable Pressure Gradient on Supersonic Turbulent Boundary Layer

    Joel J. Luker;Rodney D. W. Bowersox;Thomas A. Buter

  • Vibrationally excited NO tagging by NO(A^2Σ^+) fluorescence and quenching for simultaneous velocimetry and thermometry in gaseous flows

    Unknown

  • Sonic Injection into a Mach 5.0 Freestream Through Diamond Orifices

    Rodney D. W. Bowersox;Huaiguo Fan;Daina Lee

  • Extension of equilibrium turbulent heat flux models to high-speed shear flows

    Rodney D. W. Bowersox

  • Leading-Edge Flow Structure of a Dynamically Pitching NACA 0012 Airfoil

    B. J. Pruski;R. D. W. Bowersox

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