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About this nonfiction
Effects of Wing-crank, Leading-edge Chord Extensions and Horizontal-tail Height on the Longitudinal Stability of Swept-wing Models at Mach Numbers from 0.6 to 1.4 by Wakefield, Roy M. 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
- Wakefield, Roy M.
- Publisher
- National Aeronautics and Space Administration, [1959]
- Published
- 1959
- Language
- EN
- Category
- nonfiction
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