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Richter, Kai und Gardner, Anthony Donald und Park, Soo Hyung (2014) Numerical Investigation of the Influence of the Model Installation on Rotor Blade Airfoil Measurements. In: New Results in Numerical and Experimental Fluid Mechanics IX Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 124. Springer Verlag, Cham Heidelberg New York Dordrecht London. Seiten 225-233. doi: 10.1007/978-3-319-03158-3_23. ISBN 978-3-319-03157-6. ISSN 1612-2909.
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Offizielle URL: http://link.springer.com/chapter/10.1007/978-3-319-03158-3_23
Kurzfassung
For the assessment of the aerodynamic performance of helicopter rotor blade airfoils, accurate wind tunnel measurements of the undisturbed airfoil flow around the airfoil model are necessary. Three-dimensional CFD simulations were performed for the subsonic flow around a rotor blade airfoil model in the adaptive-wall test section of the Transonic Wind Tunnel Göttingen to investigate the influence of different types of model installations. The results revealed that the strength of the side-wall influence depends on the model installation and that a small gap between the wind tunnel model and the side wall changes the flow at the junction of model and side wall significantly.
| elib-URL des Eintrags: | https://elib.dlr.de/80717/ | ||||||||||||||||||||||||||||
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| Dokumentart: | Beitrag im Sammelband | ||||||||||||||||||||||||||||
| Zusätzliche Informationen: | DOI: 10.1007/978-3-319-03158-3_23, Online ISBN: 978-3-319-03158-3, ISSN 1860-0824 (electronic), Library of Congress Control Number: 2013957123 | ||||||||||||||||||||||||||||
| Titel: | Numerical Investigation of the Influence of the Model Installation on Rotor Blade Airfoil Measurements | ||||||||||||||||||||||||||||
| Autoren: |
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| Datum: | 2014 | ||||||||||||||||||||||||||||
| Erschienen in: | New Results in Numerical and Experimental Fluid Mechanics IX | ||||||||||||||||||||||||||||
| Referierte Publikation: | Ja | ||||||||||||||||||||||||||||
| Open Access: | Nein | ||||||||||||||||||||||||||||
| Gold Open Access: | Nein | ||||||||||||||||||||||||||||
| In SCOPUS: | Nein | ||||||||||||||||||||||||||||
| In ISI Web of Science: | Nein | ||||||||||||||||||||||||||||
| Band: | 124 | ||||||||||||||||||||||||||||
| DOI: | 10.1007/978-3-319-03158-3_23 | ||||||||||||||||||||||||||||
| Seitenbereich: | Seiten 225-233 | ||||||||||||||||||||||||||||
| Herausgeber: |
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| Verlag: | Springer Verlag, Cham Heidelberg New York Dordrecht London | ||||||||||||||||||||||||||||
| Name der Reihe: | Notes on Numerical Fluid Mechanics and Multidisciplinary Design | ||||||||||||||||||||||||||||
| ISSN: | 1612-2909 | ||||||||||||||||||||||||||||
| ISBN: | 978-3-319-03157-6 | ||||||||||||||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||||||||||||||
| Stichwörter: | TAU, DNW-TWG, side wall interference, gap, OA209 | ||||||||||||||||||||||||||||
| HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||||||||||
| HGF - Programm: | Luftfahrt | ||||||||||||||||||||||||||||
| HGF - Programmthema: | Drehflügler (alt) | ||||||||||||||||||||||||||||
| DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||||||||||
| DLR - Forschungsgebiet: | L RR - Drehflüglerforschung | ||||||||||||||||||||||||||||
| DLR - Teilgebiet (Projekt, Vorhaben): | L - Der virtuelle Drehflügler (alt) | ||||||||||||||||||||||||||||
| Standort: | Göttingen | ||||||||||||||||||||||||||||
| Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Hubschrauber | ||||||||||||||||||||||||||||
| Hinterlegt von: | Richter, Kai | ||||||||||||||||||||||||||||
| Hinterlegt am: | 28 Mär 2014 14:46 | ||||||||||||||||||||||||||||
| Letzte Änderung: | 18 Mär 2024 11:55 |
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