The use of conical camber to produce flow attachment at the leading edge of a delta wing and to minimize life-dependent drag at sonic and supersonic speeds /

The use of conical camber to produce flow attachment at the leading edge of a delta wing and to minimize life-dependent drag at sonic and supersonic speeds /

Bibliographic Details
Main Author: Smith, Jeremy H. B.
Other Authors: Mangler, K. W.
Format: Book
Language:English
Published: London : Her Majesty's Stationery Office, 1963.
Series:Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 3289.
Subjects:
Camber (Aerofoils)
Airplanes > Wings, Triangular.

Evans: Library Stacks

Holdings details from Evans: Library Stacks
Call Number: TL526.G7 A4 no. 3289
 
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TL526.G7 A4 no. 3289 Available