| Title: | An experimental pressure-distribution investigation of interference effects produced at a Mach number of 3.11 by wedge- shaped bodies located under a triangular wing / |
| Author: | Hasel, Lowell E. |
| Author: | Langley Research Center |
| Note: | Washington D.C. : National Aeronautics and Space Administration, 1959 |
| 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: | Fighter planes |
| Subject: | Aerodynamic load |
| Subject: | Airplanes |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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