Report ties in with investigation on inlet diffusers by P.RUDEN; theory of 2-dimensional diffusers extended to cover variations in inlet velocity ratio and to permit consideration of additional diffuser shapes; study of nose shapes optimum with regard to minimization of induced velocity peaks. English translation from (ZWB) Forschungsbericht n 1475/1 and 2 Sept 20 1941.
Theory of plane, symmetrical intake diffusers
Nat Advisory Committee Aeronautics -- Tech Memo
1950
76 pages
Report
English
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