Contour corrections, small in comparison with boundary-layer thickness, produce flow changes which cannot be adequately described by simple theory of characteristics; procedure involving use of experimentally determined jack influences was successfully applied to correction of nozzle profiles in 12-in. supersonic wind tunnel; considerations of further application of this method.
Correction of flexible plate supersonic nozzle contours by influence methods
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 22 , n 5 ; p 289-296
1955
8 pages
Article (Journal)
English
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Flexible nozzle for small supersonic wind tunnel
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