| Title: | Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds |
| Author: | Blair, A. B. |
| Author: | Langley Research Center |
| Author: | United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch |
| Note: | National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980 |
| 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: | Guided missiles -- Wings |
| Subject: | Rolling (Aerodynamics) |
| Subject: | Stability of airplanes, Lateral |
| Subject: | Supersonic wind tunnels |
| Subject: | Yawing (Aerodynamics) |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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