| Title: | Longitudinal stability and control characteristics from a flight investigation of a cruciform canard missile configuration having an exposed wing-canard area ratio of 16:1 |
| Author: | Moul, Martin T. |
| Author: | Wineman, Andrew R. |
| Author: | Langley Aeronautical Laboratory |
| Author: | United States. National Adviosry Committee for Aeronautics |
| Note: | National Advisory Committee for Aeronautics, 1952 |
| 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: | Rockets (Aeronautics) -- Canard fins |
| Subject: | Stability of airplanes, Longitudinal |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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