| Title: | Design and tests of a six-stage axial-flow compressor having a tip speed of 550 feet per second and a flat operating characteristic at constant speed |
| Author: | Westphal, Willard R. |
| Author: | Maynard, John W. |
| Author: | Langley Aeronautical Laboratory |
| Author: | United States. National Advisory Committee for Aeronautics |
| Note: | National Advisory Committee for Aeronautics, 1958 |
| 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 compressors -- Blades |
| Subject: | Axial flow compressors -- Design and construction |
| Subject: | Compressors -- Performance |
| Subject: | Compressors -- Testing |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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