Advantage of swept back wing as compared to normal rectangular wing is in lower drag coefficients at higher Mach numbers; attempt made to show that propeller design by incorporating recent advances in theoretical and experimental airfoil design will continue to find application in modern high speed aircraft.
Notes on propellers with swept back tips
Am Helicopter
American Helicopter ; 6 , n 5
1947
2 pages
Aufsatz (Zeitschrift)
Englisch
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