In view of amount of material on linearized treatment of axially symmetric flow, both on subsonic and supersonic regime, and because of complexity of results, it was thought advisable to work out example that, by its very simplicity, would give basic "feeling" for behavior of bodies in axially symmetric flow.
On some special problems in linearized axially symmetric flow
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 18 , n 2
1951
12 pages
Article (Journal)
English
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Engineering Index Backfile | 1950
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