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About this nonfiction
Aerodynamic characteristics of a delta wing with leading edge swept back 45 degrees, aspect ratio 4, and NACA 65A006 airfoil section. Transonic-bump method by Sleeman, William C. 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
- Sleeman, William C.
- Publisher
- National Advisory Committee for Aeronautics, 1949.
- Published
- 1949
- Language
- EN
- Category
- nonfiction
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