| Title: | Effects of spoiler-slot-deflector control on the aerodynamic characteristics at a mach number of 2.01 of a variable-wing-sweep configuration with the outer wing panels swept back 75° |
| Author: | Foster, Gerald V. |
| Author: | United States. National Aeronautics and Space Administration |
| Note: | National Aeronautics and Space Administration, 1960 |
| 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: | Aerodynamics, Supersonic |
| Subject: | Airplanes -- Wings, Swept-back |
| Subject: | Spoilers (Airplanes) -- Performance |
| Subject: | Stability of airplanes |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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