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Volumn 7, Issue , 2006, Pages 5207-5219

Aeroelastic solutions using the time accurate and non-linear frequency domain methods

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; COMPUTATIONAL EFFICIENCY; FREQUENCY DOMAIN ANALYSIS; NONLINEAR ANALYSIS; TRANSONIC FLOW; TWO DIMENSIONAL;

EID: 34250893251     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-445     Document Type: Conference Paper
Times cited : (7)

References (13)
  • 1
    • 0021523168 scopus 로고
    • Technical Report 86869
    • NASA Technical Memorandum, November
    • J. Adamczyk. Model equation for simulating flows in multistage turbomachinery. Technical Report 86869, NASA Technical Memorandum, November 1984.
    • (1984)
    • Adamczyk, J.1
  • 3
    • 34250796269 scopus 로고    scopus 로고
    • S. S. Davis. NACA 64A010 (NASA Ames model) oscillatory pitching. AGARD Report 702, August 1982. In Compendium of Unsteady Aerodynamic Measurements.
    • S. S. Davis. NACA 64A010 (NASA Ames model) oscillatory pitching. AGARD Report 702, August 1982. In Compendium of Unsteady Aerodynamic Measurements.
  • 4
    • 30744454584 scopus 로고    scopus 로고
    • Time spectral method for periodic unsteady computations over two- and three-dimensional bodies
    • AIAA paper 2000-1220, Reno, Nevada, January
    • A. Gopinath and A. Jameson. Time spectral method for periodic unsteady computations over two- and three-dimensional bodies. AIAA paper 2000-1220, 43rd Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 2005.
    • (2005) 43rd Aerospace Sciences Meeting and Exhibit
    • Gopinath, A.1    Jameson, A.2
  • 5
    • 34250873983 scopus 로고    scopus 로고
    • K. C. Hall, J. P. Thomas, and W. S. Clark. Computation of unsteady nonlinear flows in cascades using a harmonic balance technique. Technical report, 9th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines, Lyon, France, September 2000.
    • K. C. Hall, J. P. Thomas, and W. S. Clark. Computation of unsteady nonlinear flows in cascades using a harmonic balance technique. Technical report, 9th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines, Lyon, France, September 2000.
  • 6
    • 0018493237 scopus 로고
    • Transonic dip mechanism of flutter of a sweptback wing: Part ii
    • January
    • K. Isogai. Transonic dip mechanism of flutter of a sweptback wing: Part ii. AIAA Journal, 19, January 1979.
    • (1979) AIAA Journal , vol.19
    • Isogai, K.1
  • 7
    • 0003655741 scopus 로고
    • Numerical solutions of the Euler equations by finite volume methods with Runge-Kutta time stepping schemes
    • AIAA paper 81-1259, January
    • A, Jameson, W. Schmidt, and E. Turkel. Numerical solutions of the Euler equations by finite volume methods with Runge-Kutta time stepping schemes. AIAA paper 81-1259, January 1981.
    • (1981)
    • Jameson, A.1    Schmidt, W.2    Turkel, E.3
  • 8
    • 85086615843 scopus 로고    scopus 로고
    • Acceleration of convergence to a periodic steady state in turbomachinery flows
    • Reston, Va, January, American Institute of Aeronautics and Astronautics
    • M. McMullen, A. Jameson, and J. Alonso. Acceleration of convergence to a periodic steady state in turbomachinery flows. In 39th Aerospace Sciences Meeting and Exhibit, Reston, Va, January 2001. American Institute of Aeronautics and Astronautics.
    • (2001) 39th Aerospace Sciences Meeting and Exhibit
    • McMullen, M.1    Jameson, A.2    Alonso, J.3
  • 9
    • 84894380533 scopus 로고    scopus 로고
    • Application of a non-linear frequency domain solver to the euler and navier-stokes equations
    • Reston, Va, January, American Institute of Aeronautics and Astronautics
    • M. McMullen, A. Jameson, and J. Alonso. Application of a non-linear frequency domain solver to the euler and navier-stokes equations. In 40th Aerospace Sciences Meeting and Exhibit, Reston, Va, January 2002. American Institute of Aeronautics and Astronautics.
    • (2002) 40th Aerospace Sciences Meeting and Exhibit
    • McMullen, M.1    Jameson, A.2    Alonso, J.3
  • 12
    • 84894608334 scopus 로고    scopus 로고
    • S. Nadarajah, M. McMullen, and A. Jameson. Optimum shape design for unsteady flows using time accurate and non-linear frequency domain methods. In 16th AIAA Computational Fluid Dynamics Conference, Reston, Va, June 2003. American Institute of Aeronautics and Astronautics.
    • S. Nadarajah, M. McMullen, and A. Jameson. Optimum shape design for unsteady flows using time accurate and non-linear frequency domain methods. In 16th AIAA Computational Fluid Dynamics Conference, Reston, Va, June 2003. American Institute of Aeronautics and Astronautics.


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.