| Title: | Effect of several tail configurations on the stability characteristics of a midwing supersonic-bomber model at mach numbers of 1.60, 1.90, 2.20, and 2.50 |
| Author: | Wells, R. Franklin |
| Author: | Silvers, H. Norman |
| Author: | Langley 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 -- Tail surfaces -- Stability |
| Subject: | Supersonic bombers -- Design and construction |
| Subject: | Supersonic bombers -- Models |
| Subject: | Supersonic planes -- Handling characteristics |
| Subject: | Supersonic planes -- Performance |
| Subject: | Wind tunnels -- Flow visualization |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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