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Volumn , Issue , 2000, Pages

Reduced order models for nonlinear unsteady aerodynamics

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; FLIGHT DYNAMICS; FLUTTER (AERODYNAMICS); FREQUENCY DOMAIN ANALYSIS;

EID: 85087600761     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-4785     Document Type: Conference Paper
Times cited : (6)

References (24)
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  • 2
    • 0029277237 scopus 로고
    • Wing Flutter Boundary Prediction Using Unsteady Euler Aerodynamic Method
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    • Eigen-Mode Analysis in Unsteady Aerodynamics Reduced Order Models
    • New Orleans, LA, April, AIAA-95-1450
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    • Dowell, E.H.1
  • 5
    • 0001134482 scopus 로고    scopus 로고
    • Reduced-Order Models Based on Linear and Nonlinear Aerodynamic Impulse Response
    • Williamsburg, VA, June
    • Silva W. A. Reduced-Order Models Based on Linear and Nonlinear Aerodynamic Impulse Response. In International Forum on Aeroelasticity and Structural Dynamics, pages 369-379, Williamsburg, VA, June 1999.
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    • Silva, W.A.1
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    • Application of Nonlinear Systems Theory to Transonic Unsteady Aerodynamic Responses
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    • Silva, W.A.1
  • 8
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    • Extension of a Nonlinear System Theory to General-Frequency Unsteady Transonic Aerodynamic Responses
    • La Jolla, CA, April, AIAA-93-1590
    • Silva W. A. Extension of a Nonlinear System Theory to General-Frequency Unsteady Transonic Aerodynamic Responses. In 34th Structures, Structural Dynamics, and Materials Conference, La Jolla, CA, April 1993. AIAA-93-1590.
    • (1993) 34th Structures, Structural Dynamics, and Materials Conference
    • Silva, W.A.1
  • 9
    • 84983110887 scopus 로고    scopus 로고
    • Identification of Linear and Nonlinear Aerodynamic Impulse Response Using Digital Filter Techniques
    • New Orleans, LA, August, AIAA-97-3712
    • Silva W. A. Identification of Linear and Nonlinear Aerodynamic Impulse Response Using Digital Filter Techniques. In AIAA Atmospheric Flight Mechanics Conference, New Orleans, LA, August 1997. AIAA-97-3712.
    • (1997) AIAA Atmospheric Flight Mechanics Conference
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  • 11
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    • Reisenthel, P.H.1    Bettencourt, M.T.2
  • 12
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    • Modern Wing Flutter Analysis by Computational Fluid Dynamics Method
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  • 23
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.