| Title: | Distributed educated throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60-percent internal contraction |
| Author: | Shaw, Robert J. (Robert Joseph), 1946- |
| Author: | Sanders, Bobby W. |
| Author: | Mitchell, Glenn A. |
| Author: | Lewis Research Center |
| Note: | National Aeronautics and Space Administration ;, 1974 |
| 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: | Air flow |
| Subject: | Air intakes |
| Subject: | Airplanes -- Turbojet engines -- Air intakes |
| Subject: | Data acquisition |
| Subject: | Data processing |
| Subject: | Flow geometry |
| Subject: | Flow stability |
| Subject: | Inlet flow |
| Subject: | Shock waves |
| Subject: | Supersonic flow |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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