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About this nonfiction
Experimental pressure distributions over wing tips at Mach number 1.9. [Part] 2, Wing tip with subsonic trailing edge by Mirels, Harold. is a nonfiction available to read on EtoBox.
It is typically read by self-directed learners exploring a subject in depth.
Common subject areas: history, science, philosophy, social sciences.
- Author
- Mirels, Harold.
- Publisher
- National Advisory Committee for Aeronautics, [1949]
- Published
- 1949
- Language
- EN
- Category
- nonfiction
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