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Volumn 37, Issue 2, 2000, Pages 313-318

Nonlinear design loads for maneuvering elastic aircraft

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ALGORITHMS; COMPRESSIBLE FLOW; FLUID STRUCTURE INTERACTION; FUSELAGES; NAVIER STOKES EQUATIONS; TURBULENT FLOW; VISCOSITY OF LIQUIDS; VISCOUS FLOW; WINGS;

EID: 0033894750     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2595     Document Type: Article
Times cited : (23)

References (18)
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  • 3
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  • 4
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    • AIAA, Washington, DC
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    • Proceedings of the 23rd Structures, Structural Dynamics, and Materials Conference , vol.2 , pp. 267-276
    • Whitlow W., Jr.1    Bennett, R.M.2
  • 6
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    • Combined nonlinear aerodynamic and structural method for the aeroelastic design of a three-dimensional wing in supersonic flow
    • AIAA, Washington, DC
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  • 7
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    • Tatum, K.E.1    Giles, G.L.2
  • 10
    • 85002537808 scopus 로고
    • Static aeroelastic analysis of fighter aircraft using a three-dimensional Navier-Stokes algorithm
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  • 11
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    • Application of a Navier-Stokes aeroelastic method to improve fighter wing performance at maneuver flight conditions
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  • 13
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    • Convergence acceleration of Navier-Stokes solver for efficient static aeroelastic computations
    • Obayashi, S., and Guruswamy, G. P., "Convergence Acceleration of Navier-Stokes Solver for Efficient Static Aeroelastic Computations," AIAA Journal, Vol. 33, No. 6, 1996, pp. 1134-1141.
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    • Obayashi, S.1    Guruswamy, G.P.2
  • 15
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  • 16
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  • 17
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    • Navier-Stokes calculations for rotating configurations: Implementation for rockets
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    • Yaniv, S.1
  • 18
    • 0015291061 scopus 로고
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    • Harder, R.L.1    Desmarais, R.N.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.