Synonyme wurden verwendet für: Subsonic tunnels wind
Suche ohne Synonyme: keywords:(Subsonic wind tunnels)

1–10 von 10 Ergebnissen
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    Space Shuttle General Dynamics/Convair Space Shuttle Booster. Investigation of Subsonic Stability and Control Effectiveness

    W. Zombek | NTIS | 1970
    Schlagwörter: Wind tunnel stability tests , Subsonic speed , Wind tunnel models

    SPACE SHUTTLE MDAC/MMC SPACE SHUTTLE BOOSTER DETERMINATION OF STABILITY AND CONTROL CHARACTERISTICS AND POWER EFFECTS AT SUBSONIC SPEED, MACH NUMBERS ZERO AND 0.26

    D. Michna / E. Lays / C. Finch et al. | NTIS | 1971
    Schlagwörter: Low speed wind tunnels , Subsonic speed , Wind tunnel stability tests , Wind tunnel models

    Space Shuttle Verification of Booster Transition Characteristics for Transonic and Supersonic Mach Numbers (M Equals 0.6 - 5.0)

    W. V. Carter / R. F. Mcginnis | NTIS | 1971
    Schlagwörter: Wind tunnel stability tests , Subsonic speed , Wind tunnel models

    SPACE SHUTTLE INVESTIGATION OF LATERAL AND LONGITUDINAL STATIC STABILITY CHARACTERISTICS OF THE MSC ORBITERS S-1 AND S-5 AT MACH NUMBERS 0.25

    NTIS | 1971
    Schlagwörter: Low speed wind tunnels , Subsonic speed , Wind tunnel stability tests

    Aerodynamic Characteristics of Gd B-15B Booster During Cruise and Landing M Equals 0.2

    J. J. Walker / E. Burns / W. H. Gallaher | NTIS | 1971
    Schlagwörter: Subsonic speed , Wind tunnel models

    Ballute Stabilization for Various Munition Configurations. Book 2

    J. J. Graham | NTIS | 1972
    Schlagwörter: Subsonic flow , Wind tunnel models , Subsonic characteristics

    Space Shuttle Subsonic Longitudinal and Lateral-Directional Stability Investigation of the MDAC Lcr Orbiter, Unpowered and Powered

    R. Mann / P. J. Seeney / J. E. Williams | NTIS | 1971
    Schlagwörter: Subsonic wind tunnels , Wind tunnel stability tests

    Space Shuttle Aerodynamic Characteristics of the Nr delta Wing Orbiter, M Equals 0.6 to 1.3

    C. D. Andrews | NTIS | 1971
    Schlagwörter: Subsonic speed , Wind tunnel models

    Space Shuttle Determination of the Static Stability Characteristics of the 0.00285-Scale MDAC Parallel Burn Launch Configuration

    K. L. Blackwell / D. G. Lane | NTIS | 1971
    Schlagwörter: Subsonic speed , Wind tunnel stability tests