Transonic Flutter Simulation for Wing-Pylon-Nacelle Configuration Using Navier-Stokes Equations-Reference-Cited by-同舟云学术

Transonic Flutter Simulation for Wing-Pylon-Nacelle Configuration Using Navier-Stokes Equations

Published:2008-04-07 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference <br> 16th AIAA/ASME/AHS Adaptive Structures Conference<br> 10t
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Author:

Arizono Hitoshi,Kheirandish Hamid Reza,Nakamichi Jiro,Morino Hiroyuki

Publisher

American Institute of Aeronautics and Astronautics

Reference13 articles.

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2. Figure 8. Time histories of generalized displacement responses for inviscid simulations (M = 0:85;α = 0◦) tions of a Twin-Engine Transport Flutter Model in the Transonic Dynamics Tunnel,” Proceedings of International Forum on Aeroelasticity and Structural Dynamics 2003, 2003.

3. 3Soda, A. and Voss, R. “Analysis of Transonic Aerodynamic Interference in the Wing-Nacelle Region for a Generic Transport Aircraft,” Proceedings of International Forum on Aeroelasticity and Structural Dynamics 2005, 2005.

4. 4Voss,R.,Kreissl,M.,Nitzsche,J.,Soda,A.,Grisval,J.P.,andDugeai,A.“UnsteadyTransonicWingNacelleInterference for Different Oscillatory Motions,” Proceedings of International Forum on Aeroelasticity and Structural Dynamics 2007, 2007.

5. 5Dietz, G., Mai, H., Schröder, A., Klein, C., Moreaux, N., and Leconte, P. “Unsteady Wing-Pylon-Nacelle Interference in Transonic Flow,” Proceedings of 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2007.

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4. Transonic Flutter Simulation for Wing-Pylon-Nacelle Configuration Using Navier-Stokes Equations;49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference <br> 16th AIAA/ASME/AHS Adaptive Structures Conference<br> 10t;2008-04-07