| Title: | Effects of wing incidence on the longitudinal trim characteristics of a cambered 70 degree delta-wing configuration at mach numbers 3.0 to 5.0 |
| Alternate title: | Effects of wing incidence on the longitudinal trim characteristics of a cambered 70° delta-wing configuration at mach numbers 3.0 to 5.0 |
| Author: | Ahtye, Warren F. |
| Author: | Ames Research Center |
| Note: | National Aeronautics and Space Administration, 1960 |
| Link: | page images at HathiTrust |
| No stable link: | This is an uncurated book entry from our extended bookshelves, readable online now but without a stable link here. You should not bookmark this page, but you can request that we add this book to our curated collection, which has stable links. |
| Subject: | Airplanes -- Wings, Triangular -- Testing |
| Subject: | Delta wing airplanes -- Stability -- Testing |
| Subject: | Fighter planes -- Safety measures -- Testing |
| Subject: | Stability of airplanes, Longitudinal -- Testing |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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