Synonyme wurden verwendet für: Meeting
Suche ohne Synonyme: title: 42nd AIAA Aerospace Sciences Meeting and Exhibit

61–70 von 70 Ergebnissen
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    Lessons Learned in the High-Speed Aerodynamic Research Programs of the NACA/NASA

    Spearman, M. Leroy | NTRS | 2004
    compressed and there are changes in the density, pressure and temperature of the air. These compressibility effects change the aerodynamic ...
    Verlag: NASA National Aeronautics and Space Administration

    Engineering the Future of Full-Scale Propulsion Testing

    Ryan, H. M. / Solano, W. / Holland, R. et al. | NTRS | 2001
    major test facilites for large-scale propulsion devices, and summarizes the varied nature of the recent test projects conducted at the Stennis ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Spacecraft Propulsion And Power

    Results from a Sting Whip Correction Verification Test at the Langley 16-Foot Transonic Tunnel

    Crawford, B. L. / Finley, T. D. | NTRS | 2002
    tunnel models. This error source is commonly referred to as 'sting whip' and is caused by aerodynamically induced forces imparting dynamics on ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Research And Support Facilities (Air)

    Revalidation of the NASA Ames 11-by 11-Foot Transonic Wind Tunnel with a Commercial Airplane Model

    Kmak, Frank J. / Hudgins, M. / Hergert, D. et al. | NTRS | 2001
    , productivity, and reliability. Wind tunnel tests to demonstrate the readiness of the tunnel for a return to production operations included an ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Research And Support Facilities (Air)

    Some Aviation Growth Events

    Spearman, M. Leroy | NTRS | 2002
    influence of the war itself; the events during the post-war years including the establishment of aeronautical research laboratories; and the ...
    Verlag: NASA National Aeronautics and Space Administration

    Floating Potential Probe Langmuir Probe Data Reduction Results

    Morton, Thomas L. / Minow, Joseph I. | NTRS | 2002
    densities and temperatures in the ISS orbit. In this paper, the algorithms for data reduction are presented, and comparisons are made of FPP data ...
    Verlag: NASA National Aeronautics and Space Administration

    An Airplane Design having a Wing with Fuselage Attached to Each Tip

    Spearman, Leroy M. | NTRS | 2001
    having a single fuselage with cantilevered wing panels attached to the sides and tail surfaces attached at the rear. Progressively increasing the ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Aircraft Design, Testing And Performance

    Flow-Tagging Velocimetry for Hypersonic Flows Using Fluorescence of Nitric Oxide

    Danehy, P. M. / OByrne, S. / Houwing, A. F. P. | NTRS | 2001
    oxide molecules with a laser beam and then, after some delay, acquiring an image of the displaced line. One component of velocity is determined ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Fluid Mechanics And Thermodynamics

    Computation of External Aerodynamics for a Canard Rotor/Wing Aircraft

    Pandya, S. A. / Aftosmis, M. J. | NTRS | 2001
    complete rotation. A Cartesian mesh approach is used to compute the flow field about a configuration with faired-over engine inlet and exhaust that ...
    Verlag: NASA National Aeronautics and Space Administration

    Aerodynamic Performance of an Active Flow Control Configuration Using Unstructured-Grid RANS

    Joslin, Ronald D. / Viken, Sally A. | NTRS | 2001
    discontinuities at the leading edge due to the implementation of a fluidic actuator and aft of mid chord oil the upper surface. This paper documents two ...
    Verlag: American Institute of Aeronautics and Astronautics