| Title: | Design and experimental investigation of a single-stage turbine with a rotor entering relative Mach number of 2 |
| Author: | Moffitt, Thomas P. |
| Author: | Lewis Flight Propulsion Laboratory |
| Author: | United States. National Adviosry 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: | Aerodynamics, Supersonic -- Testing |
| Subject: | Airplanes -- Testing |
| Subject: | Turbines -- Aerodynamics -- Testing |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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