| Title: | Effects of wall cooling and angle of attack on boundary-layer transition on sharp cones at M[mathematical symbol for infinity] = 7.4 |
| Author: | Mateer, George G. |
| Author: | United States. National Aeronautics and Space Administration |
| Author: | Ames Research Center |
| Note: | National Aeronautics and Space Administration ;, 1972 |
| 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: | Boundary layer |
| Subject: | Cone -- Aerodynamics |
| Subject: | Heat -- Transmission |
| Subject: | Laminar flow |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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