A proper orthogonal decomposition technique for the computation of nonlinear panel response

41st Structures, Structural Dynamics, and Materials Conference and Exhibit

Volumn , Issue , 2000, Pages

  Mortara, Sean A ^a   Slater, Joseph C ^a   Beran, Philip S ^b  

^a Wright State University   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DIFFERENTIAL EQUATIONS; INTEGRAL EQUATIONS; INTEGRATION; PRINCIPAL COMPONENT ANALYSIS; STATE SPACE METHODS; STRUCTURAL DYNAMICS;

FINITE DIFFERENCE APPROACH; LOSS OF ACCURACY; MODEL REDUCTION TECHNIQUES; NONLINEAR PANEL FLUTTER; NONLINEAR STRUCTURAL DYNAMICS; PROPER ORTHOGONAL DECOMPOSITION TECHNIQUES; PROPER ORTHOGONAL DECOMPOSITIONS; SYSTEM OF EQUATIONS;

NONLINEAR EQUATIONS;

EID: 85088720318     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-1396     Document Type: Conference Paper

References (7)

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3. Romanowski, M.C., Reduced Order Unsteady Aerodynamic and Aeroelastic Models Using Karhunen-Loeve Eigen-modes., Proceedings of the 6th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Bellvue, WA, Sept., 1996, AIAA 96-3981-CP, pp. 7-13.
4. Holmes, P., Lumley, J., and Berkooz, G., Turbulence, Coherent Structures, Dynamical Systems and Symmetry, Cambridge University Press, 1996.
5. Park, H. and Lee, M., "An Efficient Method for Solving the Navier-Stokes Equations for Flow Control, " International Journal for Numerical Methods in Engineering, Vol. 41,1998, pp. 1133-1151.
6. Hall, K., Thomas, J., and Dowell, E., "Reduced-Order Modelling of Unsteady Small-Disturbance Flows Using a Frequency-Domain Proper Orthogonal Decomposition Technique, " AIAA 99-0655, Jan. 1999.
7. Beran, P.S., Huttsel, L.J., Buxton, B.J., Noll, C., and Osswald, G., Computational Aeroelasticity Techniques for Viscous Flow, Presented at the CEAS/AIAA/ICASE/NASA LaRC International Forum on Aeroelasticity and Structural Dynamics, Williamsburg, VA, June, 1999.