| Title: | Performance of a Mach Number 3.0 design axisymmetric double-cone external-compression inlet in the mach number range 1.97 to 0.79 |
| Author: | Davis, Owen H. |
| Author: | Mitchell, Glenn A. |
| Author: | Lewis 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: | Aerodynamics, Supersonic |
| Subject: | Air intakes |
| Subject: | Drag (Aerodynamics) |
| Subject: | Graphs (charts) |
| Subject: | Inlet flow |
| Subject: | Jet engines -- Air intakes |
| Subject: | Mach number |
| Subject: | Performance tests |
| Subject: | Supersonic inlets |
| Subject: | Supersonic wind tunnels |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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