Synonyms were used for: tunnels wind
Search without synonyms: keywords:(Hypervelocity wind tunnels)

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    Test Facilities of the Dfvlr in the Transonic and Hypersonic Speed Range and Main Activities

    W. Lorenz-meyer | NTIS | 1971
    Keywords: Hypervelocity wind tunnels , Transonic wind tunnels

    Free-flight testing in high-speed wind tunnels

    Dayman, B., Jr. | NTRS | 1966
    Keywords: HYPERVELOCITY WIND TUNNEL

    Aerodynamic facilities

    NTRS | 1967
    Keywords: WIND TUNNEL STABILITY TEST , HYPERVELOCITY WIND TUNNEL

    Inventory of the Principal European Wind Tunnels Capable of Being Used for Aerodynamic Tests in the Post APOLLO Programme

    J. Brocard | NTIS | 1970
    Keywords: Hypervelocity wind tunnels , Low density wind tunnels , Subsonic wind tunnels , Supersonic wind tunnels , Transonic wind tunnels

    Wind Tunnels. January, 1972-January, 1981 (Citations from the International Aerospace Abstracts Data Base)

    NTIS | 1981
    Keywords: Wind tunnels , Wind tunnel models , Hypervelocity wind tunnels , Subsonic wind tunnels , Supersonic wind tunnels , Transonic wind tunnels

    Wind Tunnels. January, 1976-January, 1981 (Citations from the Energy Data Base)

    NTIS | 1981
    Keywords: Wind tunnels , Wind tunnel models , Hypervelocity wind tunnels , Subsonic wind tunnels , Supersonic wind tunnels , Transonic wind tunnels

    Space Shuttle Aerodynamic Heating to the Grumman Space Shuttle Orbiters (Ros-NB1 and Ros-WB1) at Mach Number 8.0

    A. Derrico | NTIS | 1971
    Keywords: Hypervelocity wind tunnels , Wind tunnel models

    Test-Facilities of the Dfvlr in the Transonic and Hypersonic Speed-Range and Main Activities

    W. Lorenz-meyer | NTIS | 1971
    Keywords: Hypervelocity wind tunnels , Transonic wind tunnels

    Femtosecond Laser Electronic Excitation Tagging Velocimetry in a Large-Scale Hypersonic Facility

    Dogariu, Laura E. / Dogariu, Arthur / Miles, Richard B. et al. | AIAA | 2019
    Keywords: Hypervelocity Wind Tunnels

    Technique Development for Investigating Axisymmetric Ablation Models in Hypersonic Impulse Facilities

    Odion Iyinomen, Daniel / Malpress, Ray / Buttsworth, David | AIAA | 2021
    Keywords: Hypervelocity Flow , Hypersonic Wind Tunnels

    Effects of Shock-Tube Cleanliness on Hypersonic Boundary Layer Transition at High Enthalpy

    Jewell, Joseph S. / Parziale, Nicholaus J. / Leyva, Ivett A. et al. | AIAA | 2016
    Keywords: Hypervelocity Wind Tunnels

    Supersaturation Total Temperature, Pitot Pressure, and Rayleigh Scattering Measurements at Mach 10

    Balla, R. Jeffrey / Rhode, Matthew N. / Everhart, Joel L. | AIAA | 2014
    Keywords: Hypervelocity Wind Tunnels

    Standard Ballistic Heads Hb-1 and Hb-2 Summary Report on Aerodynamic Characteristics from Mach 2 to Mach 16.5

    R. Ceresuela | NTIS | 1968
    Keywords: Hypervelocity wind tunnels , Hotshot wind tunnels , Wind tunnel stability tests

    Results of Pressure Distribution Tests of a 0.010-Scale Space Shuttle Orbiter Model (61-0) in the NASA/Arc 3.5-Foot Hypersonic Wind Tunnel (Test OH38), Volume 3

    W. H. Dye / T. Polek | NTIS | 1975
    Keywords: Hypervelocity wind tunnels , Wind tunnel apparatus , Wind tunnel tests

    Shock Train/Boundary-Layer Interaction in Rectangular Isolators

    Geerts, Jonathan S. / Yu, Kenneth H. | AIAA | 2016
    Keywords: Hypervelocity Wind Tunnels

    Results of Pressure Distribution Tests of a 0.010-Scale Space Shuttle Orbiter Model (61-0) in the NASA/Arc 3.5-Foot Hypersonic Wind Tunnel (Test OH38), Volume 1

    W. H. Dye / T. Polek | NTIS | 1975
    Keywords: Hypervelocity wind tunnels , Wind tunnel apparatus , Wind tunnel tests

    Direct Numerical Simulation Database for Supersonic and Hypersonic Turbulent Boundary Layers

    Zhang, Chao / Duan, Lian / Choudhari, Meelan M. | AIAA | 2018
    Keywords: Hypervelocity Wind Tunnels

    Global Temperature-Sensitive Paint System for Heat Transfer Measurements in Long-Duration Hypersonic Flows

    Kurits, Inna / Lewis, Mark J. | AIAA | 2009
    Keywords: Hypersonic Shock Tunnel , Hypervelocity Wind Tunnels

    Results of Pressure Distribution Tests of a 0.010-Scale Space Shuttle Orbiter Model (61-0) in the NASA/Arc 3.5-Foot Hypersonic Wind Tunnel (Test OH38), Volume 2

    W. H. Dye / T. Polek | NTIS | 1975
    Keywords: Hypervelocity wind tunnels , Wind tunnel apparatus , Wind tunnel tests