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2011 | Nr 11 (220) | 148--160
Tytuł artykułu

Metoda numerycznej analizy aerosprężystości

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Warianty tytułu
Aeroelastic computations for aircraft model for flutter analysis based on GVT model
Języki publikacji
In this paper fluid-structure interaction, taking into account the nonlinearity of structural models, is concerned. Aeroelastic simulation of model aircraft based on GVT model configuration presents the capability of used numerical codes to analyze large-scale complex geometries. All computations were carried out in parallel environment for CFD mesh of order of millions tetrahedral elements.

Opis fizyczny
Bibliogr. 15 poz., fot., rys., schem., tab., wzory
  • Politechnika Poznańska
  • Politechnika Poznańska
  • Politechnika Poznańska
  • Politechnika Poznańska
  • Politechnika Poznańska
  • Politechnika Poznańska
  • Politechnika Poznańska
  • [1] Posadzy P., Morzyński M., Deliverable D5.2-24 - Final report on functionality of the implemented generic CSM code (Milestone M8), Poznań, August 2004.
  • [2] Kamakoti R., Computational Aeroelasticity Using a Pressure-Based Solver, Florida 2004.
  • [3] Bisplingoff R. L., Ashley H.( Halfman R. L.( Aeroelasticity, Dover, New York 1955.
  • [4] Atluri S. N., Shen S. The Meshless local Petrov-Galerkin (MLPG) Method: A Simple & Less-Costly Alternative to the Finite Element & Bounduary Element Method, CMES: Computer Modeling In Engineering & Sciences, vol. 3, n. 1, pp. 11-52, 2002.
  • [5] Guruswamy, G. P., Byun, C, Fluid-Structure Interactions Using Navier-Stokes Flow equations Coupled with Shell Finite Element Structures, AIAA-93-3087,1993.
  • [6] Bisplingoff R. L., Ashley H., Halfman R. L., Aeroelasticity, Dover, New York 1955.
  • [7] Farhat C, High Performance Computational Aeroelasticity, Boulder, USA, 2003.
  • [8] MpCCI, Book of Abstracts, 3rd User Forum February 27th & 28th, Germany, Frankfurt. 2002.
  • [9] TAURUS Project final meeting: Technical Achievements in the Software Tools Developed at EADS-CASA, Amsterdam 2003.
  • [10] Patil M. J., Hodges D. H. - On the Importance of Aerodynamic and Structural Geometrical Nonliearities in Aeroelastic Behavior of High-Aspect Ratio Wings, AIAA-00-1448, 2000.
  • [11] MpCCI, Innovative Simulation Technology, Background Information, Germany, Frankfurt 2000.
  • [12] Li Z., Parallel Computations of 3d Unsteady Compressible Euler Equations with Structural Coupling, Indianapolis 2002.
  • [13] Muller T., Lawerenz M., Shape Adaptive Airfoil for Turbomachinery applications: Simulations and Optimization, Kassel, Germany, 2004.
  • [14] Morton S. A., Melville R. B., Visbal M. R. - Accuracy and Coupling Issues of Aeroelastic Navier-Stokes Solutions on Deforming Meshes - Journal of Aircraft, vol. 25, no. 5, September-October 1999, pp. 798-805.
  • [15] Farhat C, Degand B., Koobus B., Lesoinne M. - An Improved Method of Spring Analogy for Dynamic Unstructured Fluid Meshes - AIAA 98-2070, April 1998.
Praca badawcza finansowana ze środków projektu: UDA-POIG.01.03.01-160/08-00
Typ dokumentu
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