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Volumn 8, Issue , 2006, Pages 5818-5840

Treatment of complex configurations for flutter calculations

Author keywords

CFD; Computational aeroelasticity

Indexed keywords

AIRCRAFT; COMPUTER SIMULATION; FLUID DYNAMICS; WINGS;

EID: 34147188577     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (3)

References (26)
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    • Numerical Study of Control Surface Buzz Using Computational Fluid Dynamics Methods
    • AIAA Paper 92-2654, June
    • Fuglsang, D.F., Brase, L.O. and Agarwal, S. A Numerical Study of Control Surface Buzz Using Computational Fluid Dynamics Methods, 10th AIAA Appied Aerodynamics Conference, AIAA Paper 92-2654, June, 1992.
    • (1992) 10th AIAA Appied Aerodynamics Conference
    • Fuglsang, D.F.1    Brase, L.O.2    Agarwal, S.A.3
  • 8
    • 85003265857 scopus 로고
    • Some contributions on a control surface buzz at high subsonic speeds
    • Y. Nakamura. Some contributions on a control surface buzz at high subsonic speeds. Journal of Aircraft, Vol.5(2):pp. 118, 1968.
    • (1968) Journal of Aircraft , vol.5 , Issue.2 , pp. 118
    • Nakamura, Y.1
  • 9
    • 34147187662 scopus 로고
    • Effects of Reynolds number and frequency parameter on control surface buzz at high subsonic speeds
    • Y. Nakamura and L. Woodgate. Effects of Reynolds number and frequency parameter on control surface buzz at high subsonic speeds. Aeronautical Research Council R & M, No. 3702, 1972.
    • (1972) Aeronautical Research Council R & M , Issue.3702
    • Nakamura, Y.1    Woodgate, L.2
  • 11
    • 0018998714 scopus 로고
    • Calculation of transonic aileron buzz
    • J. L. Steger and H. E. Bailey. Calculation of transonic aileron buzz. AIAA Journal, Vol.18(3):pp. 249-255, 1980.
    • (1980) AIAA Journal , vol.18 , Issue.3 , pp. 249-255
    • Steger, J.L.1    Bailey, H.E.2
  • 12
    • 34147156608 scopus 로고
    • A suggested method for analyzing for transonic flutter of control surfaces based on available data
    • A. L. Erickson and J. D. Stephenson. A suggested method for analyzing for transonic flutter of control surfaces based on available data. NACA RM A7F30, 1947.
    • (1947) NACA RM A7F30
    • Erickson, A.L.1    Stephenson, J.D.2
  • 14
    • 0037866715 scopus 로고    scopus 로고
    • Aileron buzz simulation using an implicit multiblock aeroelastic solver
    • G. Yang and S. Obayashi. Aileron buzz simulation using an implicit multiblock aeroelastic solver. Journal of Aircraft, Vol.40(3):pp. 580-589, 2003.
    • (2003) Journal of Aircraft , vol.40 , Issue.3 , pp. 580-589
    • Yang, G.1    Obayashi, S.2
  • 15
    • 48749145864 scopus 로고
    • Upwind Schemes and Boundary Conditions with Applications to Euler Equations in General Geometries
    • Osher, S. and Chakravarthy, S. Upwind Schemes and Boundary Conditions with Applications to Euler Equations in General Geometries. Journal of Computational Physics, Vol. 50, pp 447-481, 1983.
    • (1983) Journal of Computational Physics , vol.50 , pp. 447-481
    • Osher, S.1    Chakravarthy, S.2
  • 16
    • 34249988639 scopus 로고
    • Towards the Ultimate Conservative Conservative Difference Scheme II: Monotonicity and Conservation Combined in a Second Order Scheme
    • Van Leer, B. Towards the Ultimate Conservative Conservative Difference Scheme II: Monotonicity and Conservation Combined in a Second Order Scheme. Journal Computational Physics, Vol 14, 361-374, 1974.
    • (1974) Journal Computational Physics , vol.14 , pp. 361-374
    • Van Leer, B.1
  • 17
    • 0004261656 scopus 로고
    • Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings
    • AIAA Paper 91-1596
    • Jameson, A. Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings. AIAA Paper 91-1596, 1991
    • (1991)
    • Jameson, A.1
  • 18
    • 0343228755 scopus 로고    scopus 로고
    • Elements of Computational Fluid Dynamics on Block Structured Grids using Implicit Solvers
    • Badcock, K.J., Richards, B.E. and Woodgate, M.A. Elements of Computational Fluid Dynamics on Block Structured Grids using Implicit Solvers. Progress in Aerospace Sciences, vol 36, 2000, pp 351-392.
    • (2000) Progress in Aerospace Sciences , vol.36 , pp. 351-392
    • Badcock, K.J.1    Richards, B.E.2    Woodgate, M.A.3
  • 19
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    • Construction of curvilinear coordinate systems amd applications to mesh generation
    • Gordon, W.J. and Hall, C.A. Construction of curvilinear coordinate systems amd applications to mesh generation. Int J Num Meth Engr, 7, 1973, pp 461-477.
    • (1973) Int J Num Meth Engr , vol.7 , pp. 461-477
    • Gordon, W.J.1    Hall, C.A.2
  • 22
    • 34147183168 scopus 로고    scopus 로고
    • Tamayama, M., Saitoh, K., Matsushita, H. and Nakamichi, J. NAL Arrow Wing with Oscillating Flap, Verification an Validation Data for Computational Unsteady Aerodynamics, RTO Technical Report-26, October, 2000, 295-318.
    • Tamayama, M., Saitoh, K., Matsushita, H. and Nakamichi, J. NAL Arrow Wing with Oscillating Flap, Verification an Validation Data for Computational Unsteady Aerodynamics, RTO Technical Report-26, October, 2000, 295-318.
  • 24
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    • Treatment of Forced Flap Motions for Aeroelastic Simulations of an Arrow Wing
    • AIAA Paper 2005-4962, Toronto
    • Rampurawala, A.M. and Badcock, K.J., Treatment of Forced Flap Motions for Aeroelastic Simulations of an Arrow Wing. AIAA Paper 2005-4962, AIAA Applied Aerodynamics Conference, Toronto, 2005.
    • (2005) AIAA Applied Aerodynamics Conference
    • Rampurawala, A.M.1    Badcock, K.J.2
  • 26
    • 22544455994 scopus 로고    scopus 로고
    • Direct Aeroelastic Bifurcation Analysis of a Symmetric Wing Based on the Euler Equations
    • Badcock, K.J., Woodgate, M.A. and Richards, B.E., Direct Aeroelastic Bifurcation Analysis of a Symmetric Wing Based on the Euler Equations, Journal of Aircraft, 42(3),731-737, 2005.
    • (2005) Journal of Aircraft , vol.42 , Issue.3 , pp. 731-737
    • Badcock, K.J.1    Woodgate, M.A.2    Richards, B.E.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.