| Title: | Study of the pressure rise across shock waves required to separate laminar and turbulent boundary layers |
| Author: | Donaldson, Coleman duP. |
| Author: | Lange, Roy H. |
| Author: | United States. National Advisory Committee for Aeronautics |
| Note: | National Advisory Committee for Aeronautics, 1952 |
| 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: | Laminar boundary layer |
| Subject: | Laminar flow |
| Subject: | Shock waves |
| Subject: | Turbulence |
| Subject: | Turbulent boundary layer |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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