Investigation of 3-dimensional shock cylinder configuration conducted in University of Michigan supersonic wind tunnel at Mach 1.90. Bibliography.
Experiments on interaction of shock waves and cylindrical bodies at supersonic speeds
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 19 , n 4 ; p 237-248
1952
12 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Flow separation ahead blunt bodies at supersonic speeds
TIBKAT | 1951
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|On transition experiments at moderate supersonic speeds
Engineering Index Backfile | 1957
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