| Title: | Stability and control characteristics at a Mach number of 1.97 of an airplane configuration having two types of variable- sweep wings |
| Author: | Foster, Gerald V. |
| Author: | Morris, Odell A. |
| Author: | Langley Research Center |
| Author: | United States. National Aeronautics and Space Administration |
| 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, Swept-back -- Testing |
| Subject: | Mach number |
| Subject: | Stability of airplanes |
| Subject: | Supersonic wind tunnels |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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