Local pressure distribution on a blunt delta wing for angles of attack up to 35 degrees at Mach numbers of 3.4 and 4.7
Marvin Kussoy
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“Local pressure distribution on a blunt delta wing for angles of attack up to 35 degrees at Mach numbers of 3.4 and 4.7” by Marvin Kussoy: a public-domain…
Catalogue details
- Author
- Marvin Kussoy
- Category
- General & Other
- Language
- English
- Source
- HathiTrust