Efficient Aeroelastic Analysis Using Unstructured CFD Method and Reduced-Order Unsteady Aerodynamic Model-Reference-Cited by-同舟云学术

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Efficient Aeroelastic Analysis Using Unstructured CFD Method and Reduced-Order Unsteady Aerodynamic Model

Published:2009-05-04 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
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Author:

Morino Hiroyuki¹,Yamaguchi Hitoshi¹,Kumano Takayasu²,Jeong Shinkyu²,Obayashi Shigeru²

Affiliation:

1. Mitsubishi Aircraft Corporation

2. Tohoku University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-2326

Reference23 articles.

1. 1Bhatia,K."AirplaneAeroelasticity:PracticeandPotential,"AIAAPaper2001-0430.

2. 2Silva,W.A.,Bartels,R.E."DevelopmentofReduced-OrderModelsforAeroelasticAnalysisandFlutterPredictionUsing theCFL3Dv6.0 Code," AIAA Paper 2002-1596.

3. 3Kim,D.H.,Park,Y.M.,Lee,I.,Kwon,O.J."NonlinearAeroelasticComputationofWingswithPylon/Finned-StoreUsing Parallel UnstructuredEulerSolver,"AIAA Paper 2002-1289.

4. 4Thomas,J.P.,Dowell,E.H.,Hall,K.C."Three-DimensionalTransonicAeroelasticityUsingProperOrthogonal DecompositionBased ReducedOrder Models,"AIAA Paper 2001-1526.

5. 5Arizono,H.,Kheirandish,H.R.,Nakamichi,J.,Morino,H."TransonicFlutterSimulationforWing-Pylon-Nacelle Configuration usingNavier-StokesEquations,"AIAA Paper2008-1987.

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1. Design Rule Extraction Using Multiobjective Design Exploration;Computational Intelligence in Aerospace Sciences;2014-05-14

2. Calculation of Unsteady Control Surface Aerodynamics using Reduced-Order Models;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04

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