Title: | Lateral-control investigation of flap-type controls on a wing with quarter-chord line sweptback 35©�, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section. Transonic-bump method |
Author: | Thompson, Robert F. |
Author: | Langley Aeronautical Laboratory |
Author: | United States. National Adviosry Committee for Aeronautics |
Author: | United States. National Advisory Committee for Aeronautics |
Note: | National Advisory Committee for Aeronautics, 1950 |
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: | Aerofoils -- Testing |
Subject: | Airplanes -- Control |
Subject: | Airplanes -- Control surfaces |
Subject: | Airplanes -- Models -- Wings |
Subject: | Airplanes -- Wings, Swept-back |
Subject: | Charts, diagrams, etc. |
Subject: | Flaps (Airplanes) |
Subject: | Wind tunnel testing |
Other copies: | Look for editions of this book at your library, or elsewhere. |
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