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Synonyms were used for: NUMBER • REYNOLDS NUMBER
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    Force and Moment Analysis for the High Reynolds Number Wind Tunnel Test of the Space Launch System at Ascent Conditions

    Patrick R. Shea / David T. Chan / Morgan A. Walker et al. | NTRS
    Keywords: High Reynolds Number Test

    Overview of the High Reynolds Number Ascent Wind Tunnel Test of the Space Launch System at the National Transonic Facility

    David Chan / Patrick Shea / Scott Goodliff et al. | NTRS
    Keywords: High Reynolds Number Test

    Dynamic similitude between a model and a full-scale body for model investigation at full-scale Mach number

    Neihouse, Anshal I / Pepoon, Philip W | NTRS | 1950
    Keywords: MACH NUMBER , REYNOLDS NUMBER

    It’s Hip To Be Square - Refurbishment of the NASA Langley National Transonic Facility Test Section Plenum Door

    Roman Paryz / Donald Saxer / Kevin Harrell | NTRS
    Keywords: Cryogenic or High Reynolds Number Tunnels

    Some Effects of Reynolds and Mach Numbers on the Lift of an NACA 0012 Rectangular Wing in the NACA 19-Foot Pressure Tunnel

    Muse, Thomas C | NTRS | 1943
    Keywords: MACH NUMBER , REYNOLDS NUMBER

    Turbulent flow of an elasticoviscous non- Newtonian fluid.

    Ernst, W. D. | NTRS | 1967
    Keywords: REYNOLDS NUMBER

    Effect of Mach and Reynolds Numbers on the Maximum Lift Coefficient Obtainable in Gradual and Abrupt Stalls of a Pursuit Airplane Equipped with a Low-Drag Wing

    Blair, William K | NTRS | 1945
    Keywords: MACH NUMBER , REYNOLDS NUMBER

    Effects of Mach Number Variation Between 0.07 and 0.34 and Reynolds Number Variation Between 0.97 x 10(exp 6) and 8.10 x 10(exp 6) Power on the Maximum Lift Coefficient of a Wing of NACA 64-210 Airfoil Sections

    Fitzpatrick, James E / Schneider, William C | NTRS | 1952
    Keywords: MACH NUMBER EFFECTS - COMPLETE WINGS , REYNOLDS NUMBER EFFECTS - COMPLETE WINGS

    Two-dimensional Aerodynamic Characteristics of 34 Miscellaneous Airfoil Sections

    Loftin, Laurence K , Jr / Smith, Hamilton A | NTRS | 1949
    Keywords: REYNOLDS NUMBER EFFECTS - WING SECTIONS

    Low-speed static longitudinal and lateral stability characteristics of two low-aspect-ratio wings cambered and twisted to provide a uniform load at a supersonic flight condition

    Fisher, Lewis R | NTRS | 1951
    Keywords: REYNOLDS NUMBER EFFECTS - COMPLETE WINGS

    Experimental Investigation of Velocity Distributions of Downstream of Single Duct Bends

    Weske, John R | NTRS | 1948
    Keywords: REYNOLDS NUMBER

    Effect of Ground Interference on the Aerodynamic Characteristics of a 42 Degrees Sweptback Wing

    Furlong, G Chester / Bollech, Thomas V | NTRS | 1951
    Keywords: REYNOLDS NUMBER EFFECTS - COMPLETE WINGS

    The Effect of Boundary-layer Control by Suction and Several High-lift Devices on the Longitudinal Aerodynamic Characteristics of a 47.5 Degree Sweptback Wing-fuselage Combination

    Pasamanick, Jerome / Proterra, Anthony J | NTRS | 1948
    Keywords: REYNOLDS NUMBER EFFECTS - COMPLETE WINGS

    Effects of Mach Number up to 0.34 and Reynolds Number up to 8 X 10(exp 6) Power on the Maximum Lift Coefficient of a Wing of NACA 66-series Airfoil Sections

    Furlong, G Chester / Fitzpatrick, James E | NTRS | 1950
    Keywords: REYNOLDS NUMBER , MACH NUMBER , REYNOLDS NUMBER EFFECTS - COMPLETE WINGS

    Effects of sweep on controls

    Lowry, John G / Axelson, John A / Johnson, Harold I | NTRS | 1948
    Keywords: MACH NUMBER EFFECTS - COMPLETE WINGS , REYNOLDS NUMBER EFFECTS - COMPLETE WINGS

    Navier-Stokes Solutions About the F/A-18 Forebody-Leading-Edge Extension Configuration

    Farhad Ghaffari / James M Luckring / James L Thomas et al. | NTRS | 1990
    Keywords: Freestream Mach Number , Reynolds Averaged Navier Stokes

    Tests in the NACA two-dimensional low-turbulence tunnel of airfoil sections designed to have small pitching moments and high lift-drag ratios

    Tetervin, Neal | NTRS | 1943
    Keywords: MACH NUMBER , REYNOLDS NUMBER

    Analysis of Available Data on Control Surfaces Having Plain-Overhang and Frise Balances

    Toll, Thomas A | NTRS | 1944
    Keywords: MACH NUMBER , REYNOLDS NUMBER

    Transonic Navier-Stokes Solutions About a Generic Hypersonic Configuration

    Farhad Ghaffari / James M Luckring / James L Thomas et al. | NTRS | 1991
    Keywords: Freestream Mach Number , Reynolds Averaged Navier Stokes

    Considerations of the total drag of supersonic airfoil sections

    Ivey, H Reese / Klunker, E Bernard | NTRS | 1947
    Keywords: REYNOLDS NUMBER

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