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Klein, Christian und Sachs, Werner und Henne, Ulrich und Engler, Rolf und Wiedemann, Andreas und Konrath, Robert (2006) Development of PSP Technique for Application on the VFE-2 65° Delta Wing Configuration. 44th AIAA Aerospace Sciences Meeting and Exhibit, 2006-01-09 - 2006-01-12, Reno, Nevada (USA). ISBN 1-56347-795-5.
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Offizielle URL: http://www.aiaa.org
Kurzfassung
For the International Vortex Flow Experiment 2 (VFE-2) new wind tunnel tests on a NASA delta-wing model by using modern non-intrusive measurement techniques have been performed in the DNW-TWG (Göttingen) transonic wind tunnel. In order to obtain a good understanding of the flow around the wind tunnel model the PSP (Pressure Sensitive Paint) technique has been applied. The PSP technique can be used to realize absolute pressure measurements on the whole surface of a model using scientific grade cameras and advanced image processing techniques. By means of the planar pressure information of the flow topology can be investigated in more detail than would be possible with data of conventional pressure taps. Surface pressures on the entire surface of the model have been obtained using DLR's mobile PSP system, viewing from top and bottom by means of four CCD-cameras. Finally, the measured pressures have been integrated to calculate forces and moments of the full model.
| elib-URL des Eintrags: | https://elib.dlr.de/21957/ | ||||||||||||||||||||||||||||
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| Dokumentart: | Konferenzbeitrag (Vortrag, Paper) | ||||||||||||||||||||||||||||
| Zusätzliche Informationen: | LIDO-Berichtsjahr=2006 5 Disc, CD Code: 778-241002 36 Folien | ||||||||||||||||||||||||||||
| Titel: | Development of PSP Technique for Application on the VFE-2 65° Delta Wing Configuration | ||||||||||||||||||||||||||||
| Autoren: |
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| Datum: | 2006 | ||||||||||||||||||||||||||||
| Referierte Publikation: | Nein | ||||||||||||||||||||||||||||
| Open Access: | Nein | ||||||||||||||||||||||||||||
| Gold Open Access: | Nein | ||||||||||||||||||||||||||||
| In SCOPUS: | Nein | ||||||||||||||||||||||||||||
| In ISI Web of Science: | Nein | ||||||||||||||||||||||||||||
| Band: | Vol. 11, No. 1-5 | ||||||||||||||||||||||||||||
| Name der Reihe: | AIAA Meeting Papers on Disc | ||||||||||||||||||||||||||||
| ISBN: | 1-56347-795-5 | ||||||||||||||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||||||||||||||
| Stichwörter: | Vortex Flow Experiment 2 (VFE-2), PSP (Pressure Sensitive Paint) | ||||||||||||||||||||||||||||
| Veranstaltungstitel: | 44th AIAA Aerospace Sciences Meeting and Exhibit | ||||||||||||||||||||||||||||
| Veranstaltungsort: | Reno, Nevada (USA) | ||||||||||||||||||||||||||||
| Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||||||||||
| Veranstaltungsbeginn: | 9 Januar 2006 | ||||||||||||||||||||||||||||
| Veranstaltungsende: | 12 Januar 2006 | ||||||||||||||||||||||||||||
| Veranstalter : | AIAA | ||||||||||||||||||||||||||||
| HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||||||||||
| HGF - Programm: | Luftfahrt | ||||||||||||||||||||||||||||
| HGF - Programmthema: | Starrflügler (alt) | ||||||||||||||||||||||||||||
| DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||||||||||
| DLR - Forschungsgebiet: | L AR - Starrflüglerforschung | ||||||||||||||||||||||||||||
| DLR - Teilgebiet (Projekt, Vorhaben): | L - Flugphysik (alt) | ||||||||||||||||||||||||||||
| Standort: | Göttingen | ||||||||||||||||||||||||||||
| Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Experimentelle Verfahren | ||||||||||||||||||||||||||||
| Hinterlegt von: | Micknaus, Ilka | ||||||||||||||||||||||||||||
| Hinterlegt am: | 19 Jun 2006 | ||||||||||||||||||||||||||||
| Letzte Änderung: | 24 Apr 2024 19:03 |
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