| Title: | Effects of sweep angle and thickness ratio on the aerodynamic characteristics in pitch at M = 2.0 |
| Alternate title: | Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effects of sweep angle and thickness ratio on the aerodynamic characteristics in pitch at M = 2.0 |
| Alternate title: | 2.0 |
| Author: | Robinson, Ross B. |
| Author: | Langley Aeronautical Laboratory |
| Author: | United States. National Adviosry Committee for Aeronautics |
| Note: | National Advisory Committee for Aeronautics, 1952 |
| 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 -- Testing |
| Subject: | Camber (Aerofoils) |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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