| Title: | The effect of a change in airfoil section on the hinge-moment characteristics of a half-delta tip control with a 60° sweep angle at a Mach number of 6.9 |
| Author: | Fetterman, David E. |
| Author: | Ridyard, Herbert W. |
| Author: | United States. National Adviosry Committee for Aeronautics |
| Author: | Langley Aeronautical Laboratory |
| Note: | National Advisory Committee for Aeronautics, 1954 |
| 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 |
| Subject: | Airplanes -- Control surfaces |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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