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Volumn , Issue , 1994, Pages

Convergence acceleration of an aeroelastic navier-stokes solver

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTICITY; FLEXIBLE WINGS; FLUID DYNAMICS; RIGID WINGS;

EID: 84997848426     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (60)

References (26)
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  • 2
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    • Oct, Errata: AIAA Journal, Vol. 30, No. 2, Feb. 1992, pp. 569
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    • (1991) AIAA Journal , vol.29 , Issue.10 , pp. 1668-1677
    • Obayashi, S.1    Guruswamy, G.P.2    Goorjian, P.M.3
  • 3
    • 0026925805 scopus 로고
    • Unsteady Shock-Vortex Interaction on a Flexible Delta Wing
    • Sept.-Oct
    • Obayashi, S. and Guruswamy, G. P., “Unsteady Shock-Vortex Interaction on a Flexible Delta Wing, “ Journal of Aircraft, Vol. 29, No. 5, Sept.-Oct. 1992, pp. 790-798.
    • (1992) Journal of Aircraft , vol.29 , Issue.5 , pp. 790-798
    • Obayashi, S.1    Guruswamy, G.P.2
  • 7
    • 0024070893 scopus 로고
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    • September
    • Yoon, S. and Jameson, A., “Lower-Upper Symmetric-Gauss-Seidel Method for the Euler and Navier-Stokes Equations, “ AIAA Journal, Vol. 26, No. 9, pp. 1025-1026, September 1988.
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  • 8
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    • Obayashi, S. and Wada, Y., “Practical Formulation of a Positively Conservative Scheme, “ to appear in AIAA Journal.
    • To Appear in AIAA Journal
    • Obayashi, S.1    Wada, Y.2
  • 10
    • 2942757053 scopus 로고
    • Approximate Riemann Solvers, Parameter Vectors, and Difference Scheme
    • Roe, P. L., “Approximate Riemann Solvers, Parameter Vectors, and Difference Scheme, “ Journal of Computational Physics, Vol. 43, pp. 357-372, 1981.
    • (1981) Journal of Computational Physics , vol.43 , pp. 357-372
    • Roe, P.L.1
  • 16
    • 0026187123 scopus 로고
    • Preconditioned Conjugate Gradient Methods for the Compressible Navier-Stokes Equations
    • July
    • Venkatakrishnan, V., “Preconditioned Conjugate Gradient Methods for the Compressible Navier-Stokes Equations, “ AIAA Journal, Vol. 29, No. 7, July 1991, pp. 1092-1100.
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  • 19
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    • Numerical Solutions of Forward-Right rotor Flow Using an Upwind Method
    • June
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  • 22
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    • Aeroelastic Time Response Analysis of Thin Airfoils by Transonic Code LTRANS2
    • Dec
    • Guruswamy, P. and Yang, T. Y., “Aeroelastic Time Response Analysis of Thin Airfoils by Transonic Code LTRANS2, “ Computers and Fluids, Vol. 9, No. 4, Dec. 1980, pp. 409-425.
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.