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  1. 161
    Aerodynamics of a transitioning turbine stator over a range of Reynolds numbers /
    by Boyle, Robert J.
    Published 1998
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  2. 162
    Design guide for aerodynamics testing of Earth and planetary entry vehicles in a ballistic range /
    by Bogdanoff, D. W. (David W.)
    Published 2017
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  3. 163
    Application of a Navier-Stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques /
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  4. 164
    NASA Glenn 1-by 1-foot supersonic wind tunnel user manual /
    by Seablom, Kirk D.
    Published 1999
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  5. 165
    Reynolds number effects on the performance of lateral control devices /
    by Mineck, Raymond E.
    Published 2000
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  6. 166
    Coherent large-scale structures in high Reynolds number supersonic jets /
    by Lepicovsky, Jan
    Published 1985
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  7. 167
    Mach 6 flow field surveys beneath the forebody of an airbreathing missile /
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  8. 168
    R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel /
    by Jenkins, Renaldo V.
    Published 1986
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  9. 169
    Aerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes /
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  10. 170
    Generation of performance model for the Aeolian Wind Tunnel (AWT) rotor at reduced pressure /
    by Koning, Witold J. F.
    Published 2018
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  11. 171
    Shared memory parallelization of an implicit adi-type cfd code /
    by Huang, P. G., Hauser, Th
    Published 1999
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  12. 172
    Effects of artificial viscosity on the accuracy of high-Reynolds-number k-e turbulence model /
    by Chitsomboon, Tawit
    Published 1994
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  13. 173
    Implicit solution of three-dimensional internal turbulent flows /
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  14. 174
    Numerical simulation of pressure-induced separation of turbulent flat-plate boundary layers : definition and overview of new cases with suction-only transpiration and a step in Reynolds Number /
    by Coleman, Gary N.
    Published 2021
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