| Title: | Effect of vertical-tail modifications on the static stability characteristics at mach number of 2.2 of a supersonic vtol airplane model having a broad fuselage and small delta wings |
| Author: | Robinson, Ross B. |
| Author: | Spearman, Leroy M. |
| 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: | Aerodynamics, Supersonic |
| Subject: | Elevators (Airplanes) |
| Subject: | Vertically rising aircraft -- Stability |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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