| Title: | NASA TN D-5393 |
| Alternate title: | Effect of jet velocity and axial location of nozzle exit on the performance of a twin-jet afterbody model at Mach numbers up to 2.2 |
| Author: | Berrier, Bobbly Lee |
| Author: | Wood, Frederick H., Jr |
| Author: | Langley Research Center |
| Author: | United States. National Aeronautics and Space Administration |
| Note: | National Aeronautics and Space Administration ;, 1969 |
| 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: | Drag (Aerodynamics) |
| Subject: | Supersonic nozzles -- Testing |
| Subject: | Supersonic wind tunnels |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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