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Volumn , Issue , 2004, Pages 11339-11359

CFD-based aeroservoelastic analysis with Hyper-X applications

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY CONDITIONS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; ELASTICITY; FINITE ELEMENT METHOD; FLOW OF FLUIDS; VISCOSITY;

EID: 2942746463     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-884     Document Type: Conference Paper
Times cited : (3)

References (12)
  • 5
    • 0023119573 scopus 로고
    • Euler solutions for transonic flow past a fighter wing
    • Sankar, L. N., Malone, J.B., and Schuster, D., "Euler Solutions for Transonic Flow Past a Fighter Wing", Journal of Aircraft, Vol. 24, No. 1, 1987, pp 10-16.
    • (1987) Journal of Aircraft , vol.24 , Issue.1 , pp. 10-16
    • Sankar, L.N.1    Malone, J.B.2    Schuster, D.3
  • 6
    • 0021285934 scopus 로고
    • A Taylor-galerkin method for convective transport problem
    • Donea, J., "A Taylor-galerkin Method for Convective Transport Problem", International Journal of Numerical Methods in Engineering, Vol. 20, No. 1, 1984, pp 101-119.
    • (1984) International Journal of Numerical Methods in Engineering , vol.20 , Issue.1 , pp. 101-119
    • Donea, J.1
  • 9
    • 0042777704 scopus 로고    scopus 로고
    • STARS - An integrated general-purpose finite element structural, aeroelastic and aeroservoelastic analysis computer program
    • May; Revised March 2003 (version 03/01)
    • Gupta, K.K., "STARS - An Integrated General-Purpose Finite Element Structural, Aeroelastic and Aeroservoelastic Analysis Computer Program," NASA TM 4795. May 1997; Revised March 2003 (version 03/01)
    • (1997) NASA TM , vol.4795
    • Gupta, K.K.1
  • 10
    • 0030245214 scopus 로고    scopus 로고
    • Development of a finite element aeroelastic analysis capability
    • Gupta, K.K., "Development of a Finite Element Aeroelastic Analysis Capability", Journal of Aircraft, Vol. 33, No. 5,1996, pp 995-1002.
    • (1996) Journal of Aircraft , vol.33 , Issue.5 , pp. 995-1002
    • Gupta, K.K.1
  • 11
    • 85086618052 scopus 로고    scopus 로고
    • Three fields based nonlinear aeroelastic simulation technology: Status and application to the flutter analysis of an F-16 configuration
    • Geuzaire, P., Brown, G, and Farhat, C., "Three Fields Based Nonlinear Aeroelastic Simulation Technology: Status and application to the Flutter Analysis of an F-16 Configuration," AIAA paper 2002-0870, 2002.
    • (2002) AIAA Paper , vol.2002 , Issue.870
    • Geuzaire, P.1    Brown, G.2    Farhat, C.3
  • 12
    • 0027205973 scopus 로고
    • Aero thermalelastic analysis of a NASP demonstrator model
    • Heeg, J., Zeiler, T., Pototzky, A., Spain, V., and Engelund, W., "Aero Thermalelastic Analysis of a NASP Demonstrator Model", AIAA paper 93-1366, 1993.
    • (1993) AIAA Paper , vol.93 , Issue.1366
    • Heeg, J.1    Zeiler, T.2    Pototzky, A.3    Spain, V.4    Engelund, W.5


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.