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.
Description
Item Description:Cover title.
Physical Description:54 pages : illustrations
Bibliography:Bibliography: page 20.