Optimized upwind dispersion-relation-preserving finite difference scheme for computational aeroacoustics

AIAA Journal

Volumn 36, Issue 11, 1998, Pages 2146-2151

  Zhuang, M ^a,b,c   Chen, R F ^a,b,d  

^a MICHIGAN STATE UNIVERSITY   (United States)

^b Department of Mechanical Engineering ^*  (United States)

^c AIAA   (United States)

^d CFD RESEARCH CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL METHODS; DAMPING; DISPERSIONS; ENERGY DISSIPATION; ERROR ANALYSIS; FINITE DIFFERENCE METHOD; OPTIMIZATION;

OPTIMIZED UPWIND DISPERSION-RELATION-PRESERVING METHOD;

AERODYNAMICS;

EID: 0032207978     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.319     Document Type: Article

References (5)

1. Lillico, M., Butler, R., Guo, S. J., and Banerjee, J. R., "Aeroelastic Optimisation of Composite Wings Using the Dynamic Stiffness Method," Aeronautical Journal, Vol. 101, No. 1002, 1997, pp. 77-86.
2. Lillico, M., Butler, R., and Holden, M., "Conceptual Design Optimization of Composite Wings with Aeroelastic and Strength Constraints," Proceedings of the AIAA/NASA/USAF 6th Symposium on Multidisciplinary Analysis and Optimization (Bellevue, WA), AIAA, Reston, VA, 1996, pp. 191-200.
3. Banerjee, J. R., and Williams, F. W., "Free Vibration of Composite Beams - An Exact Method Using Symbolic Computation," Journal of Aircraft, Vol. 32, No. 3, 1995, pp. 636-642.
4. Taylor, J. M., and Butler, R., "Optimum Design and Validation of Flat Composite Beams Subject to Frequency Constraints," AIAA Journal, Vol. 35, No. 3, 1997, pp. 540-545.
5. ANSYS User's Manual, Version 5.0, Swanson Analysis Systems Inc., Houston, PA, 1992.