| Title: | Lift-curve slopes determined in flight on a flexible swept-wing jet bomber |
| Author: | Aiken, William S., Jr |
| Author: | Fisher, Raymond A. |
| Author: | Langley Aeronautical Laboratory |
| Author: | United States. National Advisory Committee for Aeronautics |
| Note: | Washington, D.C. : National Advisory Committee for Aeronautics, [1956], 1956 |
| 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: | Acceleration (Mechanics) -- Measurement |
| Subject: | Aerodynamic load |
| Subject: | Airplanes, Military -- Bombers |
| Subject: | Airplanes -- Flight testing |
| Subject: | Airplanes -- Wings, Swept-back |
| Subject: | Angle of attack (Aerodynamics) |
| Subject: | Charts, diagrams, etc. |
| Subject: | Lift (Aerodynamics) |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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