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title: 7th aerodynamics testing conference

Synonyms were used for: Conference • Testing
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    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

    Transonic wall interference effects on bodies of revolution

    COUCH, L. | AIAA | 1972

    Thrust stand for evaluation of thrust vectoring nozzle performance

    ESKER, D. / SEDRICK, A. | AIAA | 1972

    THE HIGHWAY AERODYNAMIC TEST FACILITY

    BROWN, GLEN / SEEMANN, GERALD | AIAA | 1972

    The effect of base mounted cylinders on a near wake

    MERZ, R. / PAGE, R. / PRZIREMBEL, C. | AIAA | 1972

    The design and operation of the Air Force Flight Dynamics Laboratory Ballistic Impact Test Facility

    HODGES, J. / MANGOLD, V. / GEBHARD, C. | AIAA | 1972

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

    MARTE, J. | AIAA | 1972

    The Aero-Propulsion Systems Test Facility

    MITCHELL, J. | AIAA | 1972

    Summary of parachute wind tunnel testing methods at Sandia National Laboratories

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

    Simulation of the interaction of high altitude plumes and a high-speed free-stream flow

    HOLTZ, T. / MUNTZ, E. | AIAA | 1972

    Refinements in high-Reynolds-number shock-tunnel technology

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

    On the use of fine wire thermocouple probes in heated high speed flows

    AIAA | 1972

    Nitrogen temperature determination in arc tunnel air flows

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

    National aeronautical facilities program /NAFP/

    KAMCHI, J. / JOHNSTON, J. | AIAA | 1972

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

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

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

    PALKO, R. | AIAA | 1972

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

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

    Flow interference in a variable porosity trisonic wind tunnel

    DAVIS, J. / GRAHAM, R. | 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

    Electron beam visualization in hypersonic air flows

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

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