| Title: | Flight investigation at Mach numbers from 0.6 to 1.7 to determine drag and base pressures on a blunt-trailing-edge airfoil and drag of diamond and circular-arc airfoils at zero lift |
| Author: | Morrow, John D. |
| Author: | Katz, Ellis |
| Author: | Langley Aeronautical Laboratory |
| Author: | United States. National Adviosry Committee for Aeronautics |
| Author: | United States. National Advisory Committee for Aeronautics |
| Note: | National Advisory Committee for Aeronautics, 1950 |
| 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: | Aerodynamic load |
| Subject: | Aerodynamics, Supersonic |
| Subject: | Aerofoils -- Testing |
| Subject: | Charts, diagrams, etc. |
| Subject: | Drag (Aerodynamics) |
| Subject: | Mach number |
| Subject: | Trailing edges (Aerodynamics) |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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