Positions of boundary layer transition were ascertained for sweptback and straight wing of like conditions; sweptback wing in definite range of angle of attack resulted in backward shift of transition point on suction side of wing; favorable effect of sweepback on position of transition point predicted by LIPPISCH is confirmed. English translation from (ZWB) Deutsche Luftfahrtforschung -- U u M n 3151 Sept 13 1944.
Maintaining laminar flow in boundary layer using swept-back wing
Nat Advisory Committee Aeronautics -- Tech Memo
1948
9 pages
Article (Journal)
English
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