Design of small tunnel test section (4×10-in.) incorporating flexible nozzle; consisting of high strength stepped steel plate; two screw jacks provide easy means of continuously changing nozzle's shape according to aerodynamic requirements; boundary layer compensation can also be varied during operation.
Flexible nozzle for small supersonic wind tunnel
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 18 , n 4
1951
6 pages
Article (Journal)
English
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Asymmetric adjustable supersonic nozzle for wind-tunnel application
Engineering Index Backfile | 1953
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