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title: 7th aerodynamics testing conference

Synonyms were used for: Conference • Testing
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    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

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

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

    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

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

    POVINELLI, F. / DITTMAR, J. | 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

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

    POUNDS, G. | AIAA | 1972

    Flow interference in a variable porosity trisonic wind tunnel

    DAVIS, J. / GRAHAM, R. | AIAA | 1972

    Nitrogen temperature determination in arc tunnel air flows

    LAZDINIS, S. / CARPENTER, R. | AIAA | 1972

    Transonic wall interference effects on bodies of revolution

    COUCH, L. | AIAA | 1972

    Electron beam visualization in hypersonic air flows

    LEE, H. / PETRIE, S. | AIAA | 1972

    Electron-beam flow visualization - Applications in the definition of configuration aerothermal characteristics

    WOODS, W. / ARRINGTON, J. | AIAA | 1972

    Viking configuration pitch damping derivatives as influenced by support interference and test technique at transonic and supersonic speeds

    STEINBERG, S. / USELTON, B. / SIEMERS, III, P. | AIAA | 1972

    Flow quality improvements in a blowdown wind tunnel using a multiple shock entrance diffuser

    ARNOLD, J. / COOKSEY, J. | AIAA | 1972

    Refinements in high-Reynolds-number shock-tunnel technology

    HICKMAN, R. / KYSER, J. | AIAA | 1972

    Aerodynamics of high-performance Ludwieg tubes

    RUSSELL, D. | AIAA | 1972

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