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Factors affecting transition at supersonic speeds
Content Provider | HathiTrust Digital Library |
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Author | Czarnecki, K. R Sinclair, Archibald R |
Editor | K. R. Czarnecki Archibald R. Sinclair |
Organization | United States. National Advisory Committee for Aeronautics. |
Description | This paper surveys the available material and summarizes what is known to date about boundary-layer transition at supersonic speeds. Variables studied include Mach number, Reynolds number, pressure gradients, heat transfer, surface roughness, and angle of attack. The discussion is limited to bodies of revolution because similar reliable data for wings is lacking |
Volume Number | L53I18A |
Language | English |
Publisher | National Advisory Committee for Aeronautics |
Publisher Date | 1953-01-01 |
Publisher Place | Washington D.C. |
Access Restriction | Open |
Rights License | Items in this record are available as Public Domain, Google-digitized. View the access and use profile at http://www.hathitrust.org/access_use#pd-google. Please see individual items for rights and use statements |
Subject Keyword | Turbulence Charts, diagrams, etc Aerodynamics, Supersonic Surfaces (Physics) Boundary layer Laminar flow |
Content Type | Text |
Resource Type | Book |