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General & OtherLocal pressure distribution on a blunt delta wing for angles of attack up to 35 degrees at Mach numbers of 3.4 and 4.7Marvin KussoyLocal pressure distribution on a blunt delta wing for angles of attack up to 35 degrees at Mach numbers of 3.4 and 4.7

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

About this book

“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” is a book by Marvin Kussoy in the “General & Other” category, written in English. It is in the public domain, so you can read it for free from the open source using the buttons above. If you enjoyed it, press Like to help others find it. Similar books are listed below.

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