General & OtherExperimental pressure distributions over wing tips at Mach number 1.9. [Part] 2, Wing tip with subsonic trailing edgeHarold Mirels![Experimental pressure distributions over wing tips at Mach number 1.9. [Part] 2, Wing tip with subsonic trailing edge]()
Experimental pressure distributions over wing tips at Mach number 1.9. [Part] 2, Wing tip with subsonic trailing edge
Harold Mirels
Al-Warraq Library does not host book files; it takes you to the copy at the original source. Public-domain status differs from country to country, so check the law where you live before downloading or republishing the book. Do you hold rights in this work? Request its removal
“Experimental pressure distributions over wing tips at Mach number 1.9. [Part] 2, Wing tip with subsonic trailing edge” by Harold Mirels: a public-domain…
Catalogue details
- Author
- Harold Mirels
- Category
- General & Other
- Language
- English
- Source
- HathiTrust