| Title: | Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86 |
| Author: | Lamb, Milton |
| 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 ;, 1981 |
| 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 -- Aerodynamics -- Testing |
| Subject: | Guided missiles -- Control systems -- Testing |
| Subject: | Wind tunnels -- Testing |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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