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    AIAA 7th Aerodynamic Testing Conference : Palo Alto, CA, September 13 - 15, 1972

    American Institute of Aeronautics and Astronautics | TIBKAT | 1972

    I112 Wind Tunnel Testing on Crosswind Aerodynamic Forces Acting on Railway Vehicles

    Kwon, H.-b. / Nam, S.-w. / You, W.-h. et al. | British Library Conference Proceedings | 2008

    I112 Wind Tunnel Testing on Crosswind Aerodynamic Forces Acting on Railway Vehicles

    Kwon, H.-b. / Nam, S.-w. / You, W.-h. et al. | British Library Conference Proceedings | 2008

    The design and operation of a large tube-vehicle aerodynamic testing facility

    MARTE, J. | AIAA | 1972

    THE HIGHWAY AERODYNAMIC TEST FACILITY

    BROWN, GLEN / SEEMANN, GERALD | AIAA | 1972

    Full-scale inlet/engine testing at high maneuvering angles at transonic velocities

    PALKO, R. | AIAA | 1972

    Development of the AEDC-VKF tunnel J - A real gas high density, true velocity, hypersonic, aerodynamic test facility

    PATE, S. / SILER, L. / STALLINGS, D. et al. | AIAA | 1972

    Characteristics of an ejector-type engine simulator for STOL model testing

    NICOLOFF, G. / WEBER, H. | AIAA | 1972

    A modular asymmetric parachute for wind tunnel testing

    KLIMAS, P. / WIDDOWS, H. / CROLL, R. | AIAA | 1981

    Summary of parachute wind tunnel testing methods at Sandia National Laboratories

    CROLL, R. / KLIMAS, P. / TATE, R. et al. | AIAA | 1981

    Investigations of the Influence of Lower Frequency Aerodynamic Noise on Interior Cruise and Exterior Pass-By Sound Levels

    Donavan, Paul R. | SAE Technical Papers | 2012
    additional pass-by testing using different tires on a variety of pavements. It was further found that aerodynamic noise was likely a partial ...

    Computation of wall effects in ventilated transonic wind tunnels

    MURMAN, E. | AIAA | 1972

    A comparison of disturbance levels measured in hypersonic tunnels using a hot-wire anemometer and a pitot pressure probe

    STAINBACK, P. / WAGNER, R. | AIAA | 1972

    The Aero-Propulsion Systems Test Facility

    MITCHELL, J. | AIAA | 1972

    Design and development of the United Aircraft Research Laboratories acoustic research tunnel

    PATERSON, R. / VOGT, P. / FOLEY, W. | AIAA | 1972

    The high Reynolds number cryogenic wind tunnel

    GOODYER, M. / KILGORE, R. | AIAA | 1972

    Installation caused flow distortion and its effect on noise from a fan designed for turbofan engines

    POVINELLI, F. / DITTMAR, J. | AIAA | 1972

    Evaluation of transonic and supersonic wind-tunnel background noise and effects of surface pressure fluctuation measurements

    DODS, JR., J. / HANLY, R. | AIAA | 1972

    An initial two-dimensional wall interference investigation in a transonic wind tunnel with variable porosity test section walls

    POUNDS, G. | AIAA | 1972

    Factors affecting phase-change paint heat-transfer data reduction with emphasis on wall temperatures approaching adiabatic conditions

    STONE, D. / HARRIS, J. / THROCKMORTON, D. et al. | AIAA | 1972

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