| Title: | Rocket-model investigation of longitudinal stability and drag characteristics of an airplane configuration have a 60° delta wing and a high unwept horizontal tail |
| Author: | Peck, Robert F. |
| Author: | Mitchell, Jesse L. |
| Author: | Langley Aeronautical Laboratory |
| Author: | United States. National Advisory Committee for Aeronautics |
| Note: | Washington, D.C. : National Advisory Committee for Aeronautics, 1953., 1953 |
| 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: | Delta wing airplanes |
| Subject: | Stability of airplanes, Longitudinal |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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