Calculations of the steady conical flow past a yawed slender delta wing with leading-edge separation /

Calculations of the steady conical flow past a yawed slender delta wing with leading-edge separation /

Bibliographic Details
Main Author: Pullin, D. I.
Corporate Author: Aeronautical Research Council (Great Britain)
Format: Book
Language:English
Published: London : Her Majesty's Stationery Office, 1975.
Series:Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 3767.
Subjects:
Airplanes > Wings, Triangular.
Leading edges (Aerodynamics)

Evans: Library Stacks

Holdings details from Evans: Library Stacks
Call Number: TL526.G7 A4 no. 3767
 
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TL526.G7 A4 no. 3767 Available