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Volumn , Issue , 2001, Pages

Simulation of transonic limit cycle oscillations using a CFD time-marching method

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTICITY; COMPUTATIONAL FLUID DYNAMICS; MESSAGE PASSING;

EID: 85067321815     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-1290     Document Type: Conference Paper
Times cited : (14)

References (20)
  • 4
    • 0001106389 scopus 로고
    • Semi-Empirical Unsteady Aerodynamics for Modeling Aircraft Limit Cycle Oscillations and Other Nonlinear Aeroelastic Problems
    • Manchester, U.K., Jun
    • Cunningham Jr., A.M. and Meijer, J.J., "Semi-Empirical Unsteady Aerodynamics for Modeling Aircraft Limit Cycle Oscillations and Other Nonlinear Aeroelastic Problems," International Forum on Aeroelasticity and Structural Dynamics, Manchester, U.K., Jun. 1995.
    • (1995) International Forum On Aeroelasticity and Structural Dynamics
    • Cunningham, A.M.1    Meijer, J.J.2
  • 7
    • 0033715583 scopus 로고    scopus 로고
    • Mesh Strategies for Accurate Computation of Unsteady Spoiler and Aeroelastic Problems
    • Bartels, R.E., "Mesh Strategies for Accurate Computation of Unsteady Spoiler and Aeroelastic Problems," Journal of Aircraft, Vol. 37, pp.521-525, 2000.
    • (2000) Journal of Aircraft , vol.37 , pp. 521-525
    • Bartels, R.E.1
  • 8
    • 84894469384 scopus 로고    scopus 로고
    • http://finadwww.larc.nasa.gov/biedron/Cfl3dv6/cfl3dv6.html
  • 15
    • 2942757053 scopus 로고
    • Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes
    • Roe, P.L., "Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes," Journal of Computational Physics, Vol. 43, pp.357-372, 1981.
    • (1981) Journal of Computational Physics , vol.43 , pp. 357-372
    • Roe, P.L.1
  • 19
    • 0020846613 scopus 로고
    • Time-Marching Transonic Flutter Solutions Including Angle-of-Attack Effects
    • Edwards, J.W., Bennett, R.M., Whitlow, W. Jr., and Seidel, D.A., "Time-Marching Transonic Flutter Solutions Including Angle-of-Attack Effects," Journal of Aircraft, Vol. 20, pp.899-906, 1983.
    • (1983) Journal of Aircraft , vol.20 , pp. 899-906
    • Edwards, J.W.1    Bennett, R.M.2    Whitlow Jr., W.3    Seidel, D.A.4
  • 20
    • 0024091975 scopus 로고
    • Modern Wing Flutter Analysis by Computational Fluid Dynamics Methods
    • Cunningham, H.J., Batina, J.T., and Bennett, R.M., "Modern Wing Flutter Analysis by Computational Fluid Dynamics Methods," Journal of Aircraft, Vol. 25, pp.962-968, 1988.
    • (1988) Journal of Aircraft , vol.25 , pp. 962-968
    • Cunningham, H.J.1    Batina, J.T.2    Bennett, R.M.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.