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

1–20 von 109 Ergebnissen
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    Human Missions to Mars Key Challenges

    B. G. Drake | NTIS | 2013
    Schlagwörter: Delta launch vehicle

    Status of Aquarius/SAC-D

    D. M. Le Vine | NTIS | 2011
    Schlagwörter: Delta launch vehicle

    Sting Influence on Vortex Breakdown on a 65 Degree Delta Wing in Transonic Flow

    L. A. Schiavetta / R. M. Cummings / O. J. Boelens et al. | NTIS | 2007
    Schlagwörter: Delta wings

    Computational and Physical Aspects of UAV Vortical Flows

    M. R. Visbal | NTIS | 2004
    Schlagwörter: Delta wings

    Vortex Flows at Supersonic Speeds

    R. M. Wood / F. J. Wilcox / S. X. S. Bauer et al. | NTIS | 2003
    Schlagwörter: Delta wings

    Overview of the Electrodynamic Delivery Express (EDDE)

    J. Pearson / J. Carroll / E. Levin et al. | NTIS | 2003
    Schlagwörter: Delta v capability

    Dynamics of Aerospace Vehicles -- Nonlinear Flight Mechanics

    J. E. Jenkins / G. A. Addington / P. S. Beran et al. | NTIS | 2000
    Schlagwörter: Delta wings

    High Speed Vortex Flows

    R. M. Wood / F. J. Wilcox / S. X. S. Bauer et al. | NTIS | 2000
    Schlagwörter: Delta wings

    Low Speed Straked Delta Wing

    E. G. Geurts | NTIS | 2000
    Schlagwörter: Delta wings

    Mars Orbit Rendezvous Strategy for the Mars 2003/2005 Sample Return Mission

    L. A. DAmario / W. E. Bollman / W. J. Lee et al. | NTIS | 1999
    Schlagwörter: Delta launch vehicle

    Analysis of Delta Wing Vortical Substructures Using Detached-Eddy Simulation

    A. Mitchell / S. Morton / J. Forsythe | NTIS | 1997
    Schlagwörter: Delta wings

    Control of Leading-Edge Vortices With Suction

    I. Gursul | NTIS | 1996
    Schlagwörter: Delta wings

    Unsteady Structure of Leading-Edge Vortices on a Delta Wing

    D. O. Rockwell | NTIS | 1994
    Schlagwörter: Delta wings

    Wind Prelaunch Mission Operations Report (MOR)

    NTIS | 1994
    Schlagwörter: Delta launch vehicle

    Flow Field over the Wing of a delta-Wing Fighter Model with Vortex Control Devices at Mach 0.6 to 1.2

    E. A. Bare / D. E. Reubush / R. C. Haddad | NTIS | 1992
    Schlagwörter: Delta wings