Synonyme wurden verwendet für: Stabilität
Suche ohne Synonyme: keywords:(Stabilität)

121–140 von 13,177 Ergebnissen
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    Wind-Tunnel Tests of a 1/4-Scale Model of the Naval Aircraft Factory Float-Wing Convoy Interceptor, TED No. NACA 2314

    Wells, Evalyn G. / McKinney, Elizabeth G. | NTRS | 1947
    Schlagwörter: Aircraft Stability And Control

    Wind-Tunnel Tests for Active Flutter Control and Closed-Loop Flutter Identification

    Huang, Rui / Zhao, Yonghui / Hu, Haiyan | AIAA | 2016
    Schlagwörter: Routh Hurwitz Stability Criterion

    Wind Tunnel Tests at Transonic and Supersonic Speeds to Investigate the Longitudinal Stability of a Model of the Avro 720 Aircraft

    E. Huntley | NTIS | 1971
    Schlagwörter: Longitudinal stability , Wind tunnel stability tests , Aircraft stability

    Wind Tunnel Test on a 1/4.622 Froude Scale, Hingeless Rotor, Tilt Rotor Model, Volume 4

    J. P. Magee | NTIS | 1976
    Schlagwörter: Stability derivatives

    Wind Tunnel Test on a 1/4.622 Froude Scale, Hingeless Rotor, Tilt Rotor Model, Volume 3

    J. P. Magee / H. R. Alexander | NTIS | 1976
    Schlagwörter: Stability derivatives

    Wind Tunnel Test on a 1/4.622 Froude Scale, Hingeless Rotor, Tilt Rotor Model, Volume 2

    J. P. Magee / H. R. Alexander | NTIS | 1976
    Schlagwörter: Stability derivatives

    Wind Tunnel Test on a 1/4.622 Froude Scale, Hingeless Rotor, Tilt Rotor Model, Volume 1

    J. P. Magee / H. R. Alexander | NTIS | 1976
    Schlagwörter: Stability derivatives

    Wind Tunnel Test of the Modified Goldschmied Model with Propulsion and Empennage: Analysis of Test Results

    F. R. Goldschmied | NTIS | 1986
    Schlagwörter: Static stability , Aerodynamic stability

    Wind Tunnel Test of the 0.015-Scale Rockwell International Space Shuttle Vehicle Orbiter in the Ames 6 by 6 Foot Supersonic Wind Tunnel

    M. D. Milam / T. J. Dziubala | NTIS | 1973
    Schlagwörter: Lateral stability , Longitudinal stability , Wind tunnel stability tests

    Wind Tunnel Test of the 0.010-Scale Space Shuttle Integrated Vehicle in the NASA-Ames 3.5 Foot Hypersonic Wind Tunnel (IA10)

    F. F. Fitzgerald / M. T. Petrozzi / J. W. Cleary et al. | NTIS | 1973
    Schlagwörter: Spacecraft stability , Stability derivatives

    Wind Tunnel Test of a Variable-Diameter Tiltrotor (VDTR) Model

    D. Matuska / A. Dale / P. Lorber | NTIS | 1994
    Schlagwörter: Aerodynamic stability

    Wind Tunnel Test of a Powered Tilt-Rotor Performance Model. Volume V

    J. P. Magee / R. B. Taylor / F. J. McHugh et al. | NTIS | 1971
    Schlagwörter: Stability

    Wind Tunnel Test of a Model Utilizing Vectored Thrust for In-Flight Maneuverability

    W. B. Sears / C. N. Webster | NTIS | 1972
    Schlagwörter: Stability

    Wind tunnel test of a fighter aircraft wing/store flutter suppression system: An international effort

    Hwang, C. / Johnson, E. H. / Mills, G. R. et al. | NTRS | 1980
    Schlagwörter: Aircraft Stability And Control