| Title: | Method for obtaining aerodynamic data on hypersonic configurations with scramjet exhaust flow simulation |
| Author: | Hartill, William R. |
| Author: | United States. National Aeronautics and Space Administration |
| Note: | National Aeronautics and Space Administration ;, 1977 |
| 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, Hypersonic |
| Subject: | Airplanes -- Ramjet engines -- Combustion |
| Subject: | Airplanes -- Scramjet engines |
| Subject: | Hypersonic planes -- Models -- Testing |
| Subject: | Hypersonic wind tunnels -- Equipment and supplies |
| Subject: | Jets -- Fluid dynamics |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
Help with reading books -- Report a bad link -- Suggest a new listing
Home -- Search -- New Listings -- Authors -- Titles -- Subjects -- Serials
Books -- News -- Features -- Archives -- The Inside Story
Edited by John Mark Ockerbloom (onlinebooks@pobox.upenn.edu)
OBP copyrights and licenses.