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Dtic Ada173762%3a Vortex Airfoil Interaction And Application Of Methods For Digital Fringe Analysis. by Defense Technical Information Center
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1DTIC ADA173762: Vortex-Airfoil Interaction And Application Of Methods For Digital Fringe Analysis.
By Defense Technical Information Center
The interaction of convected vortices with different airfoils was investigated in a transonic duct and a shock tube flow. Different kinks of separation and secondary vortex generation have a governing influence on airfoil-vortex interaction. Steep sound waves propagating upstream are generated at the leading edge. A system for digital processing of flow interferograms has been developed.
“DTIC ADA173762: Vortex-Airfoil Interaction And Application Of Methods For Digital Fringe Analysis.” Metadata:
- Title: ➤ DTIC ADA173762: Vortex-Airfoil Interaction And Application Of Methods For Digital Fringe Analysis.
- Author: ➤ Defense Technical Information Center
- Language: English
“DTIC ADA173762: Vortex-Airfoil Interaction And Application Of Methods For Digital Fringe Analysis.” Subjects and Themes:
- Subjects: ➤ DTIC Archive - Meier,G E - MAX-PLANCK-INST FUER STROEMUNGSFORSCHUNG GOETTINGEN (GERMANY F R) - *VORTICES - *AIRFOILS - *AERODYNAMIC NOISE - IMAGE PROCESSING - DIGITAL SYSTEMS - INTERACTIONS - ACOUSTIC WAVES - BOUNDARY LAYER - CONVECTION - VORTEX SHEDDING - PRESSURE MEASUREMENT - INTERFEROGRAMS - PROFILES - HELICOPTERS - WAVE PROPAGATION - WIND TUNNEL TESTS - WAKE - LEADING EDGES - TRANSONIC WIND TUNNELS - WEST GERMANY - SHOCK TUBES - VORTEX GENERATORS
Edition Identifiers:
- Internet Archive ID: DTIC_ADA173762
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 44.81 Mbs, the file-s for this book were downloaded 113 times, the file-s went public at Sat Feb 10 2018.
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