Numerical comparison of dynamic stall for two-dimensional airfoils and an airfoil model in the DNW-TWG (English)
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In:
Journal of the American Helicopter Society
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57
, 4
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042007/1-042007/13
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2012
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ISSN:
- Article (Journal) / Print
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Title:Numerical comparison of dynamic stall for two-dimensional airfoils and an airfoil model in the DNW-TWG
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Additional title:Numerische Simulation der dynamischen Strömungsablösung an einem zweidimensionalen Tragflügelprofil und der dreidimensionalen Umströmung eines Tragflügels in in einem Windkanal
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Contributors:Klein, A. ( author ) / Lutz, T. ( author ) / Krämer, E. ( author ) / Richter, K. ( author ) / Gardner, A.D. ( author ) / Altmikus, A.R.M. ( author )
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Published in:Journal of the American Helicopter Society ; 57, 4 ; 042007/1-042007/13
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Publisher:
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Publication date:2012
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Size:13 Seiten, 16 Bilder, 1 Tabelle, 17 Quellen
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ISSN:
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Coden:
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DOI:
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Type of media:Article (Journal)
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Type of material:Print
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Language:English
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Keywords:
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Source:
Table of contents – Volume 57, Issue 4
The tables of contents are generated automatically and are based on the data records of the individual contributions available in the index of the TIB portal. The display of the Tables of Contents may therefore be incomplete.
- 042001
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Time-Domain Approach for Acoustic Scattering of Rotorcraft NoiseLee, S. / Brentner, K.S. / Morris, P.J. et al. | 2012
- 042002
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Three-Dimensional Sound Directivity around a Helicopter Turboshaft EngineGounet, H. / Lewy, S. et al. | 2012
- 042003
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Aerodynamic Optimization Study of a Coaxial Rotor in Hovering FlightSyal, M. / Leishman, J.G. et al. | 2012
- 042004
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A Tribute to Professor Rene H. Miller: A Pioneer in Aeromechanics and Rotary Wing Flight TransportationFriedmann, P.P. / Johnson, W. / Scully, M.P. et al. | 2012
- 042005
-
A Visual Study of Vortex Instabilities in theWake of a Rotor in HoverOhanian, C.V. / McCauley, G.J. / Savas, O. et al. | 2012
- 042006
-
Prediction of Brownout Inception Beneath a Full-Scale Helicopter DownwashJasion, G. / Shrimpton, J. et al. | 2012
- 042007
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Numerical Comparison of Dynamic Stall for Two-Dimensional Airfoils and an Airfoil Model in the DNW-TWGKlein, A. / Lutz, T. / Kramer, E. / Richter, K. / Gardner, A.D. / Altmikus, A.R.M. et al. | 2012
- 045001
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Technical Note Improved Shroud Design for Rotary Wing MAV Applications Based on Computational AnalysisLakshminarayan, V.K. / Baeder, J.D. et al. | 2012
- 045002
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Technical Note Innovative Technique of Using the Radar Altimeter for Prediction of Terrain Collision ThreatsLabun, J. / Sotak, M. / Kurdel, P. et al. | 2012
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A Tribute to Professor René H. Miller: A Pioneer in Aeromechanics and Rotary Wing Flight Transportation 042004Friedmann, Peretz P et al. | 2012
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A Visual Study of Vortex Instabilities in theWake of a Rotor in Hover 042005Ohanian, Christopher V et al. | 2012
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Prediction of Brownout Inception Beneath a Full-Scale Helicopter Downwash 042006Jasion, Gregory et al. | 2012
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Time-Domain Approach for Acoustic Scattering of Rotorcraft Noise 042001Lee, Seongkyu et al. | 2012
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Numerical Comparison of Dynamic Stall for Two-Dimensional Airfoils and an Airfoil Model in the DNW-TWG 042007Klein, A et al. | 2012
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Technical Note - Innovative Technique of Using the Radar Altimeter for Prediction of Terrain Collision Threats 045002Labun, Ján et al. | 2012
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Aerodynamic Optimization Study of a Coaxial Rotor in Hovering Flight 042003Syal, Monica et al. | 2012
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Technical Note - Improved Shroud Design for Rotary Wing MAV Applications Based on Computational Analysis 045001Lakshminarayan, Vinod K et al. | 2012
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Three-Dimensional Sound Directivity around a Helicopter Turboshaft Engine 042002Gounet, Helene et al. | 2012