Experimental and Numerical Study of the Unsteady Wake of a Supercritical Airfoil in a Compressible Flow
Experimental investigations were carried out to study the wake profile of a supercritical airfoil at Mach numbers of 0.4 and 0.6 in a pitching motion. Both static and dynamic tests were conducted in a tri-sonic wind tunnel. Flow field inside the wake was measured by hot wire anemometry at downstream...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
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Departamento de Ciência e Tecnologia Aeroespacial
2019-01-01
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| Series: | Journal of Aerospace Technology and Management |
| Subjects: | |
| Online Access: | http://www.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462019000100301&lng=en&nrm=iso&tlng=en |