POD approach for unsteady aerodynamic model updating

Author:

Vetrano F.,Mastroddi F.,Ohayon R.

Publisher

Springer Science and Business Media LLC

Subject

Aerospace Engineering,Transportation

Reference26 articles.

1. Mortchelewicz, G.D.: Application of proper orthogonal decomposition to linearized Euler or Reynolds-Averaged Navier-Stokes equation. In: 47th Israel Annual Conference on Aerospace Sciences, Tel Aviv, February 2007. http://publications.onera.fr/

2. Palacios, R., Climent, H., Karlsson, A., Winzell, B.: Assessment of strategies for correcting linear unsteady aerodynamics using CFD or test results. In: International Forum of Aeroelasticity and Structural Dynamics, Madrid, June 2001

3. Giesing, J.P., Kalman, T.P., Rodden, W.P.: Correction factor techniques for improving aerodynamic prediction method. Technical report NASA CR-144967 (1976)

4. Yates, E.C.: Modified-strip-analysis method for predicting wing flutter at subsonic or hypersonic speeds. J. Aircr. 3(1), 25–29 (1966)

5. Pitt, D.M., Goodman, C.E.: Flutter calculations using Doublet Lattice Aerodynamics modified by the full potential equations. In: 28th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics and Materials Conference, Monterrey, 1987 (Paper AIAA-87-0882-CP)

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