| Title: | Pressure distribution measurements of the interference effect of the wing on the fuselage at mach numbers of 1.40 and 1.59 |
| Alternate title: | An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and a 40° sweepback : pressure distribution measurements of the interference effect of the wing on the fuselage at Mach numbers of 1.40 and 1.59 |
| Author: | Gapcynski, John P. |
| Author: | United States. National Adviosry Committee for Aeronautics |
| Author: | Langley Aeronautical Laboratory |
| Author: | Clark, James W. |
| 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: | Aerodynamic load |
| Subject: | Aerodynamics, Supersonic |
| Subject: | Airplanes -- Fuselage |
| Subject: | Airplanes -- Wings, Swept-back |
| Subject: | Fuselages |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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