| Title: | Aerodynamic damping at Mach numbers of 1.3 and 1.6 of a control surface on a two-dimensional wing by the free-oscillation method |
| Author: | Tuovila, W. J. (Weimer J.) |
| Author: | Hess, R. W. (Robert W.) |
| Author: | Langley Research Center |
| Note: | National Aeronautics and Space Administration, 1960 |
| 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: | Aircraft stability |
| Subject: | Aluminum |
| Subject: | Control surfaces |
| Subject: | Free vibration |
| Subject: | Mach number |
| Subject: | Magnesium |
| Subject: | Steels |
| Subject: | Supersonic airfoils |
| Subject: | Supersonic flutter |
| Subject: | Vibration damping |
| Subject: | Wing profiles |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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