Physical argument behind methods developed at Royal Aircraft Establishment for reducing normal pressure drag of wings of moderate or large aspect ratio in transonic flight range; potential benefits of sweep; causes for drag forces arising; means of reducing drag.
Methods of reducing transonic drag of swept-back wings at zero lift
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 61 , n 553
1957
6 pages
Article (Journal)
English
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