Welcome to the von Karman Institute for Fluid Dynamics Store

Transonic aerodynamic testing - article pay-per-view - 25€/article

Be the first to review this product

Availability: In stock


Quick Overview

Transonic aerodynamic testing

Article pay-per-view

Double click on above image to view full picture

Zoom Out
Zoom In

More Views

  • Article pay-per-view

* Required Fields



  • 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

Additional Information

Manufacturer von Karman Institute for Fluid Dynamics

Product Tags

Use spaces to separate tags. Use single quotes (') for phrases.