| Title: | Overall and blade element performance of a 1.20-pressure-ratio fan stage with rotor blades reset -5 ̊ |
| Author: | Lewis, George W., Jr |
| Author: | Moore, Royce D. |
| Author: | Osborn, Walter Martin, 1918- |
| Author: | Lewis Research Center |
| Note: | U.S. National Aeronautics and Space Administration ;, 1976 |
| 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: | Axial flow |
| Subject: | Compressors -- Blades -- Testing |
| Subject: | Engine design |
| Subject: | Performance tests |
| Subject: | Rotor blades (Turbomachinery) |
| Subject: | Short haul aircraft |
| Subject: | Turbocompressors |
| Subject: | Turbofans |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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