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Low Speed Wind Tunnel Experiments on a Delta Wing Oscillating in Pitch

Hummel, D. and Löser, T. (1998) Low Speed Wind Tunnel Experiments on a Delta Wing Oscillating in Pitch. In: 21st Congress of the International Council of the Aeronautical Sciences, 98-3.9.3. 21. ICAS Congress, Melbourne (au), 13.-18.09.1998.

Full text not available from this repository.

Abstract

Thema sind statische und dynamische Kraft- und Druckmessungen an einem Deltaflügel mit einer Vorderkantenpfeilung von 65&°. im Niedergeschwindigkeitsbereich. Es werden Ergebnisse von erzwungenen Nickschwingungen um verschiedene mittlere Anstellwinkel vorgestellt.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1999,
Title:Low Speed Wind Tunnel Experiments on a Delta Wing Oscillating in Pitch
Authors:
AuthorsInstitution or Email of Authors
Hummel, D.UNSPECIFIED
Löser, T.UNSPECIFIED
Date:1998
Journal or Publication Title:21st Congress of the International Council of the Aeronautical Sciences
Volume:98-3.9.3
Series Name:ICAS
Status:Published
Keywords:Dynamic measurements, Vortical flow, Force measurements, Pressure measurements, Delta wing, Low speed, Pitching oscillation
Event Title:21. ICAS Congress, Melbourne (au), 13.-18.09.1998
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):L - Concepts & Integration
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik
Deposited By: elib DLR-Beauftragter
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 19:55

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