Analytical derivation of inlet shapes for maximum critical speed for given inlet velocity ratios; examples of resulting inlet shapes and of application to side or under wing scoops; shapes also suitable for axially symmetrical nose inlets. English translation from (ZWB) Forschungsbericht n 1209 Apr 15 1940.
Two-dimensional symmetrical inlets with external compression
Nat Advisory Committee Aeronautics -- Tech Memo
1950
48 pages
Diagrams, Charts
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Englisch
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