| Title: | Investigation of the effect of a guide-vane-rotor combination on inlet total-pressure distortions in a compressible fluid |
| Author: | Ashby, George C. |
| Author: | Langley Research Center |
| Note: | National Aeronautics and Space Administration, 1959 |
| 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: | Compressible flow |
| Subject: | Compressors |
| Subject: | Density (mass volume) |
| Subject: | Flow distortion |
| Subject: | Guide vanes |
| Subject: | Inlet flow |
| Subject: | Inlet pressure |
| Subject: | Jet aircraft |
| Subject: | Plates (structural members) |
| Subject: | Pressure distribution |
| Subject: | Rotors |
| Subject: | Subsonic speed |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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