Cover Image

Part I: The flow pattern on a tapered swept-back wing at Mach numbers between 0.6 and 1.6. Part II: Experiments with a tapered swept-back wing of Warren 12 planform at Mach numbers between 0.6 and 1.6 /

Bibliographic Details
Main Author: Hall, Ian Murray
Other Authors: Rogers, E. W. E.
Format: Book
Language:English
Published: London : Her Majesty's Stationery Office, 1962.
Series:Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 3271.
Subjects:
Airplanes > Wings, Swept-back.
Air flow.
Aerodynamics.
Description
Item Description:Cover title.
Physical Description:159 pages : illustrations
Bibliography:Bibliography: pages 10-11, pages 68-70.