Brief survey of phenomena and problems which have arisen at National Physical Laboratory, on wings having leading edge sweeps near 50°, and without twist or spanwise change in profile; wing flow at zero, moderate and high lift is discussed in detail; effect of changing flow pattern on overall wing lift, drag, and pitching moment.
Introduction to flow about plane swept-back wings at transonic speeds
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 64 , n 596
1960
16 pages
Article (Journal)
English
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Wing section design for swept-back wings at transonic speeds
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