| Title: | NASA TR R-317 |
| Alternate title: | A numerical analysis of the use of perforated walls to control shock location and movement in an internal-compression supersonic inlet |
| Author: | Matthews, Clarence W. |
| Author: | Langley Research Center |
| Author: | United States. National Aeronautics and Space Administration |
| Note: | National Aeronautics and Space Administration ;, 1969 |
| Link: | page images at HathiTrust; US access only |
| 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: | High-speed aeronautics |
| Subject: | Shock (Mechanics) |
| Subject: | Walls -- Analysis |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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