| Title: | Aerodynamic characteristics of a wing with quarter-chord line swept back 35°, aspect ratio 6, taper ratio 0.6, and NACA 65A006 airfoil section. Transonic-bump method |
| Author: | Sleeman, William C. |
| Author: | Morrison, William D. |
| Author: | United States. National Adviosry Committee for Aeronautics |
| Author: | Langley Aeronautical Laboratory |
| Note: | National Advisory Committee for Aeronautics, 1949 |
| 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, Transonic |
| Subject: | Airplanes -- Fuselage |
| Subject: | Airplanes -- Wings |
| Subject: | Drag (Aerodynamics) |
| Subject: | Fuselages |
| Subject: | Lift (Aerodynamics) |
| Subject: | Pitching (Aerodynamics) |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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