Numerical and Experimental Modelling of Transition in a Separated Boundary Layer on the NACA63A421 Airfoil
The article deals with design and numerical calculation of a variable test section for small supersonic wind tunnel. The supersonic wind tunnel is designed to be driven by a supersonic ejector. The test section, which is in focus, is considered to by placed on its suction inlet. Schlieren method wil...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
VSB-Technical University of Ostrava
2010-12-01
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| Series: | Transactions of the VSB : Technical University of Ostrava |
| Online Access: | http://transactions.fs.vsb.cz/2010-3/1812.pdf |