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Volumn , Issue , 2008, Pages

Application of multiple methods for aeroelastic uncertainty analysis

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTIC MODELS; ANALYSIS APPROACH; ANALYTICAL PREDICTIONS; COMPUTATIONAL DEMANDS; COMPUTATIONAL TIME; ESSENTIAL DYNAMICS; FLIGHT TESTING; HIGH FIDELITY; HIGH-FIDELITY SIMULATIONS; INERTIAL FORCES; MONTE CARLO; MULTIPLE METHODS; NONLINEAR AEROELASTIC SIMULATIONS; REDUCED ORDER MODELS; RESPONSE SURFACE METHOD; ROBUST STABILITY TECHNIQUES; STOCHASTIC SIMULATIONS; TRANSONIC REGIME;

EID: 70350526721     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (8)

References (17)
  • 1
    • 85007688839 scopus 로고
    • Prediction of flutter onset speed based on flight testing at subcritical speeds
    • July-August
    • Zimmerman, N., and J. Weissenburger, "Prediction of Flutter Onset Speed Based on Flight Testing at Subcritical Speeds," Journal of Aircraft, Vol. 1, No. 4, July-August 1964, pp. 190-202.
    • (1964) Journal of Aircraft , vol.1 , Issue.4 , pp. 190-202
    • Zimmerman, N.1    Weissenburger, J.2
  • 2
    • 0012535159 scopus 로고    scopus 로고
    • The state-of-the-art of unsteady aerodynamics for high performance aircraft
    • Yurkovich, R. N., Liu, D. D., and Chen, P. C., The State-of-the-Art of Unsteady Aerodynamics for High Performance Aircraft, AIAA Paper 2001-0428.
    • AIAA Paper 2001-0428
    • Yurkovich, R.N.1    Liu, D.D.2    Chen, P.C.3
  • 3
    • 0037345147 scopus 로고    scopus 로고
    • Aeroelastic dynamic analysis of a full F-16 configuration for various flight conditions
    • Geuzaine, P., Brown, G., Harris, C., and Farhat, C., Aeroelastic Dynamic Analysis of a Full F-16 Configuration for Various Flight Conditions, AIAA Journal 41, 2003, pp. 363-371.
    • (2003) AIAA Journal , vol.41 , pp. 363-371
    • Geuzaine, P.1    Brown, G.2    Harris, C.3    Farhat, C.4
  • 4
    • 0036390834 scopus 로고    scopus 로고
    • Application of a three-field nonlinear fluid-structure formulation to the prediction of the aeroelastic parameters of an F-16 fighter
    • Farhat, C., Geuzaine, P., and Brown, G., Application of a Three-Field Nonlinear Fluid-Structure Formulation to the Prediction of the Aeroelastic Parameters of an F-16 Fighter, Computers & Fluids 32, 2003, pp. 3-29.
    • (2003) Computers & Fluids , vol.32 , pp. 3-29
    • Farhat, C.1    Geuzaine, P.2    Brown, G.3
  • 6
    • 0032689370 scopus 로고    scopus 로고
    • A finite element based modal method for determination of plate stiffnesses considering uncertainties
    • Kuttenkeuler, J., A Finite Element Based Modal Method for Determination of Plate Stiffnesses Considering Uncertainties, J. of Composite Materials 33, 1999, pp. 695-711.
    • (1999) J. of Composite Materials , vol.33 , pp. 695-711
    • Kuttenkeuler, J.1
  • 7
    • 0032092070 scopus 로고    scopus 로고
    • Aeroelastic tailoring considering uncertainties in material properties
    • Kuttenkeuler, J. and Ringertz, U., Aeroelastic Tailoring Considering Uncertainties in Material Properties, Str. Optimization 15, 1998, pp. 157-162.
    • (1998) Str. Optimization , vol.15 , pp. 157-162
    • Kuttenkeuler, J.1    Ringertz, U.2
  • 9
    • 0003703360 scopus 로고
    • Anon, National Technical Information Service, U.S. Department of Commerce, Washington, DC, Oct.
    • Anon., U.S. Standard Atmosphere, 1976, National Technical Information Service, U.S. Department of Commerce, Washington, DC, Oct. 1976.
    • (1976) U.S. Standard Atmosphere 1976


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.