Plane problem of vibrating wing in supersonic flow treated by method of acceleration potential. English translation from (ZWB) Forschungsbericht n 1903 Jan 1944.
Two-dimensional wing theory in supersonic range
Nat Advisory Committee Aeronautics -- Tech Memo
National Advisory Committee for Aeronautics -- Technical Memorandums ; Tech Memo 1238
1949
34 pages
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Two-dimensional supersonic wing theory
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