| Title: | Damping in roll of models with 45°, 60°, and 70° delta wings determined at high subsonic, transonic, and supersonic speeds with rocket -powered models |
| Author: | Sanders, E. Claude |
| Author: | United States. National Adviosry Committee for Aeronautics |
| Author: | Langley Aeronautical Laboratory |
| 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: | Airplanes -- Wings, Triangular |
| Subject: | Rolling (Aerodynamics) |
| Subject: | Stability of airplanes, Lateral |
| Subject: | Vibration (Aeronautics) -- Damping |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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