An approximate integral method for calculating the incompressible laminar boundary layer on an infinite swept wing on which velocity and suction distribution are arbitrary /

Bibliographic Details
Main Author: Pinsent, H. G.
Corporate Author: Aeronautical Research Council (Great Britain)
Other Authors: Pinsent, P. A.
Format: Book
Language:English
Published: London : Her Majesty's Stationery Office, 1962.
Series:Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 3241.
Subjects:

Remote Storage

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Call Number: TL526.G7 A4 no. 3241
 
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TL526.G7 A4 no. 3241 Available