| Title: | Wind-tunnel investigation at high subsonic speeds of the effect of spoiler profile on the lateral control characteristics of a wing-fuselage combination winter quarter-chord line swept back 32.6° and NACA 65A006 airfoil section |
| Author: | Johnson, Harold S. |
| Author: | Langley Aeronautical Laboratory |
| Author: | United States. National Advisory Committee for Aeronautics |
| Note: | Washington, D.C. : National Advisory Committee for Aeronautics, 1953., 1953 |
| 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: | Airplanes -- Wings, Swept-back |
| Subject: | Stability of airplanes, Lateral |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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