| Title: | An experimental study of the flutter of sails having a delta planform tested from a Mach number of 0.1 to a Mach number of 1.9 |
| Author: | Hess, R. W. (Robert W.) |
| Author: | Langley Research Center |
| Author: | United States. National Aeronautics and Space Administration |
| Note: | National Aeronautics and Space Administration, 1961 |
| 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: | Aerodynamics, Supersonic |
| Subject: | Aerodynamics, Transonic |
| Subject: | Airplanes -- Wings, Triangular |
| Subject: | Flutter (Aerodynamics) |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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