Domain decomposition for reduced-order modeling of a flow with moving shocks

AIAA Journal

Volumn 40, Issue 11, 2002, Pages 2360-2362

  Lucia, David J ^a   King, Paul I ^a   Beran, Philip S ^a  

^a AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY CONDITIONS; COMPUTER SIMULATION; DEGREES OF FREEDOM (MECHANICS); NOZZLES; VECTORS;

PROPER ORTHOGONAL DECOMPOSITION (POD);

SHOCK WAVES;

EID: 0036848254     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1576     Document Type: Article

References (13)

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3. Lucia, D.J., Beran, P.S., and King, R.I., "Reduced Order Modeling of an Elastic Panel in Transonic Flow," AIAA Paper 2002-1594, April 2002; also Journal of Aircraft (to be published).
4. Lucia, D.J., Beran, P.S., and King, R.I., "Reduced Order Modeling of an Elastic Panel in Transonic Flow," AIAA Paper 2002-1594, April 2002; also Journal of Aircraft (to be published).
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11. Farhat, C., Macedo, A., Lesoinne, M., Roux, F., Magoules, F., and de La Bourdonnaie, A., "Two-Level Domain Decomposition Methods with Lagrange Multipliers for the Fast Iterative Solution of Acoustic Scattering Problems," Computer Methods in Applied Mechanics and Engineering, Vol. 184, No. 2, 2000, pp. 213-241.
12. Strang, G., Introduction to Applied Mathematics, Wellesley Cambridge Press, Cambridge, MA, 1986, pp. 96-100.
13. Lucia, D.J., King, P.I., Beran, P.S., and Oxley, M.E.,"Reduced Order Modeling for a One-Dimensional Nozzle Flow with Moving Shocks," AIAA Paper 2001-2602, June 2001.