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” 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
“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 Identifiers:
- The Open Library ID: OL6530450W
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