| Title: | Effect of yaw and angle of attack on pressure recovery and mass-flow characteristics of a rectangular supersonic scoop inlet at a Mach number of 2.71 |
| Author: | Comenzo, Raymond J. |
| Author: | Mackley, Ernest A. |
| 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, 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: | Jet engines -- Air intakes |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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