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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 profi le 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 fi eld inside the wake was measured by hot wire anemometry at downstre...
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| Veröffentlicht in: | Journal of Aerospace Technology and Management |
|---|---|
| Hauptverfasser: | , |
| Format: | Artigo |
| Sprache: | Inglês |
| Veröffentlicht: |
Ministério da Defesa
2019
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| Schlagworte: | |
| Online Zugang: | https://www.redalyc.org/articulo.oa?id=309457690002 |
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