Application of high-order accurate methods to solve the computational gas dynamics and aeroacoustics problems
Author:
Publisher
Allerton Press
Subject
Aerospace Engineering
Link
http://link.springer.com/content/pdf/10.3103/S1068799811010077.pdf
Reference11 articles.
1. Tam, C.K.W. and Webb, J.C., Dispersion-Relation-Preserving Finite Difference Schemes for Computational Aeroacoustics, Journal of Computational Physics, 1993, vol. 107, no. 2, pp. 262–281.
2. Tam, C.K.W. and Shen, H., Direct Computation of Nonlinear Acoustic Pulses Using High-Order Finite Difference Schemes, Proc. of the 15th Aeroacoustics Conf., Long Beach, CA, 1993, AIAA 1993–4325.
3. Bogey, C. and Bailly, C., A Family of Low Dispersive and Low Dissipative Explicit Schemes for Computing the Aerodynamic Noise, Proc. of the 8th AIAA/CEAS Aeroacoustics Conf. and Exhibit, 2002, AIAA 2002-2509.
4. Bogey, C. and Bailly, C., A Family of Low Dispersive and Low Dissipative Explicit Schemes for Flow and Noise Computations, Journal of Computational Physics, 2004, vol. 194, no. 1, pp. 194–214.
5. Berland, J., Bogey, C., and Bailly C., Optimized Explicit Schemes: Matching and Boundary Schemes, and 4th-Order Runge-Kutta Algorithm, Proc. of the 10th AIAA/CEAS Aeroacoustics Conf., AIAA 2004-2814.
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