Cover Image

Use of camber and twist to produce low-drag delta or swept-back wings, without leading-edge singularities, at supersonic speeds /

Bibliographic Details
Main Author:	Roper, G. M.
Format:	Book
Language:	English
Published:	London : Her Majesty's Stationery Office, 1961.
Series:	Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 3196.
Subjects:	Airplanes > Wings, Swept-back. Aerodynamics, Supersonic.

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