| Title: | Aerodynamic performance and static stability at mach number 3.3 of an aircraft configuration employing three triangular wing panels and a body equal length |
| Author: | James, Carlton S. |
| 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: | Aerodynamics, Supersonic |
| Subject: | Airplanes -- Performance |
| Subject: | Supersonic planes -- Research -- United States |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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