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Source: The Open Library
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1Effect of fin leading edge sweep on shock-shock interaction at Mach 6
By Scott A. Berry
“Effect of fin leading edge sweep on shock-shock interaction at Mach 6” Metadata:
- Title: ➤ Effect of fin leading edge sweep on shock-shock interaction at Mach 6
- Author: Scott A. Berry
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - [National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - Washington, DC
“Effect of fin leading edge sweep on shock-shock interaction at Mach 6” Subjects and Themes:
- Subjects: Reynolds number - Wind tunnel tests - Leading edge sweep - Hypersonic speed - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15501765M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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