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Volumn , Issue , 2008, Pages 430-435

Active flutter control of transonic flapped wing based on CFD/CSD coupling

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIR; CONTROL EQUIPMENT; DYNAMICS; GAS DYNAMICS; MATHEMATICAL MODELS; POLARIZATION;

EID: 58049155824     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/ASC-ICSC.2008.4675399     Document Type: Conference Paper
Times cited : (4)

References (5)
  • 1
    • 24644445990 scopus 로고    scopus 로고
    • Advances in the Linear/Nonlinear Control of Aeroelastic Structural Systems
    • Librescu L., Marzocca P. "Advances in the Linear/Nonlinear Control of Aeroelastic Structural Systems", Acta Mechanica [J], 2005, 178(3-4):147-186.
    • (2005) Acta Mechanica [J] , vol.178 , Issue.3-4 , pp. 147-186
    • Librescu, L.1    Marzocca, P.2
  • 2
    • 58049188323 scopus 로고    scopus 로고
    • Robert, M.B. John W.E. An Overview of Recent Developments in Computational Aeroelasticity, AIAA Fluid Dynamics Conference, 29th, Albuquerque, NM, June 15-18, 1998, 15 p. AIAA 98-2521.
    • Robert, M.B. John W.E. "An Overview of Recent Developments in Computational Aeroelasticity", AIAA Fluid Dynamics Conference, 29th, Albuquerque, NM, June 15-18, 1998, 15 p. AIAA 98-2521.
  • 3
    • 85087600761 scopus 로고    scopus 로고
    • Daniella E. Raveh. Reduced Order Models for Nonlinear Unsteady Aerodynamic, AIAA/USAF/NASA/ISSMO Symposium on Multidisiplinary Analysis and Optimization, 8th, Long Beah, CA, Sept. 6-8.2000, 11 p. AIAA 2000-4785.
    • Daniella E. Raveh. "Reduced Order Models for Nonlinear Unsteady Aerodynamic", AIAA/USAF/NASA/ISSMO Symposium on Multidisiplinary Analysis and Optimization, 8th, Long Beah, CA, Sept. 6-8.2000, 11 p. AIAA 2000-4785.
  • 4
    • 0019533482 scopus 로고
    • Principal Component Analysis in Linar System: Controllability. Observability and Model Reduction
    • Moore B. C, "Principal Component Analysis in Linar System: Controllability. Observability and Model Reduction" IEEE Trans, Automatic Control [J], 1981, AC-26(1): 17-32.
    • (1981) IEEE Trans, Automatic Control [J] , vol.AC-26 , Issue.1 , pp. 17-32
    • Moore, B.C.1
  • 5
    • 58049144813 scopus 로고    scopus 로고
    • Jose A. Rivera, Jr.. Bryan E. Dansberry, Robert M. Bennett. Michael H. Durham, Walter A. Silva. NACA 0012 Benchmark Model Experimental Flutter Results with Unsteady Pressure Distributions, AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 33rd, Dallas, TX, Apr. 13-15, 1992, Technical Papers. Pt. 4 (A92-3445113-39). Washington, DC, American Institute of Aeronautics and Astronautics, 1992, p. 1898-1908. AIAA 92-2396.
    • Jose A. Rivera, Jr.. Bryan E. Dansberry, Robert M. Bennett. Michael H. Durham, Walter A. Silva. "NACA 0012 Benchmark Model Experimental Flutter Results with Unsteady Pressure Distributions", AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 33rd, Dallas, TX, Apr. 13-15, 1992, Technical Papers. Pt. 4 (A92-3445113-39). Washington, DC, American Institute of Aeronautics and Astronautics, 1992, p. 1898-1908. AIAA 92-2396.


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.