| Title: | NASA TN D-2030 |
| Alternate title: | Wind-tunnel investigation at high subsonic speed of the static longitudinal stability characteristics of a winged reentry vehicle having a large negatively deflected flap-type control surface |
| Author: | Fournier, Paul G. |
| Author: | Langley Research Center |
| Author: | United States. National Aeronautics and Space Administration |
| Note: | National Aeronautics and Space Administration, 1963 |
| Link: | page images at HathiTrust; US access only |
| 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: | Flaps (Airplanes) -- Testing |
| Subject: | Stability of space vehicles |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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