| Title: | Incipient- and developed-spin and recovery characteristics of a modern high-speed fighter design with low aspect ratio as determined from dynamic-model tests |
| Author: | Lee, Henry A., NASA researcher |
| Author: | Libbey, Charles E. |
| Author: | United States. National Aeronautics and Space Administration |
| Author: | Langley Research Center |
| Note: | National Aeronautics and Space Administration, 1961 |
| 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: | Aerodynamic coefficients |
| Subject: | Aircraft design |
| Subject: | Aircraft stability |
| Subject: | Dynamic models |
| Subject: | Fighter aircraft |
| Subject: | Low aspect ratio |
| Subject: | Pitching moments |
| Subject: | Stability derivatives |
| Subject: | Windtunnel tests |
| Subject: | Yawing moments |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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