Tests at a mach number of 2.0 on a rectangular, twin-duct air intake with variable geometry, situated in the flow field of a slender wing - Info and Reading Options
By M. D. Dobson
"Tests at a mach number of 2.0 on a rectangular, twin-duct air intake with variable geometry, situated in the flow field of a slender wing" was published by H.M. Stationery Off. in 1970 - London, it has 22 pages and the language of the book is English.
“Tests at a mach number of 2.0 on a rectangular, twin-duct air intake with variable geometry, situated in the flow field of a slender wing” Metadata:
- Title: ➤ Tests at a mach number of 2.0 on a rectangular, twin-duct air intake with variable geometry, situated in the flow field of a slender wing
- Author: M. D. Dobson
- Language: English
- Number of Pages: 22
- Publisher: H.M. Stationery Off.
- Publish Date: 1970
- Publish Location: London
“Tests at a mach number of 2.0 on a rectangular, twin-duct air intake with variable geometry, situated in the flow field of a slender wing” Subjects and Themes:
- Subjects: Cavities (Airplanes) - Wind tunnels
Edition Specifications:
- Pagination: 14, [22] p.
Edition Identifiers:
- The Open Library ID: OL4370742M - OL6530450W
- Library of Congress Control Number (LCCN): 78552764
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