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Transonic aerodynamic testing

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  • B.H., GOETHERT -U. TENNESSEE SPACE INSTITUTE, USA: The problem -aircraft in transonic flight
  • K.P., HARTZUIKER -NLR, NETHERLANDS: Scale effects at transonic speeds. Basic considerations
  • M., PINDZOLA -ARO INC., USA: Transonic wind tunnels
  • A.R., FELIX -MARSHALL SPACE FLIGHT CENTER, USA: Design and characteristics of high Reynolds number test facilities: the Ludwieg tube
  • E., PILTZ -TH DARMSTADT, FR GERMANY: Boundary layer effects on pressure variations in Ludwieg tubes
  • C.R., TAYLOR -RAE-BEDFORD, UK: The design of wind tunnel models for tests at transonic speeds and high Reynolds numbers
  • J.M., LEWENDON -RAE-BEDFORD, UK: Flight test techniques for a transonic aircraft
  • L.Z., DUMITRESCU -INST. FLUID MECH. & AEROSP.CONSTRUCTIONS, ROUMANIA: Experimental techniques for transonic testing in shock tubes
  • A.B., HAINES -ARA LTD, UK: Possibilities for scale effects on swept wings at high subsonic speeds

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