| Title: | Preliminary results of the flight investigation between Mach numbers of 0.80 and 1.36 of a rocket-powered model of a supersonic airplane configuration having a tapered wing with circular-arc sections and 40° sweepback |
| Author: | D'Aiutolo, Charles T. |
| Author: | Mason, Homer P. |
| Author: | United States. National Adviosry Committee for Aeronautics |
| Author: | Langley Aeronautical Laboratory |
| Note: | National Advisory Committee for Aeronautics, 1958 |
| 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: | Stability of airplanes, Longitudinal -- Testing |
| Subject: | Supersonic planes |
| Subject: | Yawing (Aerodynamics) -- Testing |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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