| Title: | Flow field analysis of aircraft configurations using a numerical solution to the three-dimensional unified supersonic/hypersonic small disturbance equations / |
| Author: | Gunness, R. C. |
| Author: | Dsylva, E. |
| Author: | Knight, C. J. |
| Author: | Langley Research Center |
| Author: | Boeing Company |
| Note: | Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 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: | Hypersonic planes |
| Subject: | Supersonic planes |
| Subject: | Finite differences |
| Subject: | Inviscid flow |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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