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Volumn 69, Issue , 2004, Pages 27-36

Survey of active aeroelastic control for flutter suppression

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AIRCRAFT; ALGORITHMS; CONTROL SYSTEMS; FINITE ELEMENT METHOD; HYDRAULICS; RISK ASSESSMENT; STRUCTURAL ANALYSIS; WINGS;

EID: 17144425773     PISSN: 07334230     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/IMECE2004-60458     Document Type: Conference Paper
Times cited : (2)

References (23)
  • 1
    • 0003628366 scopus 로고
    • A historical overview of flight flutter testing
    • Oct.
    • Kehoe, Michael W.: A Historical Overview of flight Flutter Testing. NAS A Technical Memorandum 4720, Oct. 1995.
    • (1995) NAS A Technical Memorandum , vol.4720
    • Kehoe, M.W.1
  • 5
    • 0038891236 scopus 로고    scopus 로고
    • Overview of flight flutter research at NASA Dryden
    • April
    • Brenner, Martin; Lind, Rick; Voracek, David: Overview of Flight Flutter Research at NASA Dryden, NASA TM 4792, April 1997.
    • (1997) NASA TM , vol.4792
    • Brenner, M.1    Lind, R.2    Voracek, D.3
  • 6
    • 0031139413 scopus 로고    scopus 로고
    • Robust flutter margins of an F/A-18 aircraft from aeroelastic flight data
    • May - June
    • Brenner, Martin; Lind, Rick: Robust Flutter Margins of an F/A-18 Aircraft from Aeroelastic Flight Data. Journal of Guidance, Control, and Dynamics. Vol. 20, No. 3, May - June 1997.
    • (1997) Journal of Guidance, Control, and Dynamics , vol.20 , Issue.3
    • Brenner, M.1    Lind, R.2
  • 7
    • 17144417895 scopus 로고    scopus 로고
    • Aeroservoelastic simulation of an active flexible wing wind tunnel model
    • April
    • Buttrill, Carey S.; Bacon, Barton J.; Heeg, Jennifer; Houck, Jacob A.; and Wood, David V.: Aeroservoelastic Simulation of an Active Flexible Wing Wind Tunnel Model NASA Technical Paper 3510, April 1996.
    • (1996) NASA Technical Paper , vol.3510
    • Buttrill, C.S.1    Bacon, B.J.2    Heeg, J.3    Houck, J.A.4    Wood, D.V.5
  • 11
    • 0036539271 scopus 로고    scopus 로고
    • Thermal post-buckling and aeroelastic behavior of shape memory alloy reinforced plates
    • Institute of Physics Publishing, Smart Material and Structure, Apr. 5, 2002
    • Tawfik, Mohammad; Ro, J.; Mei, Chuh: Thermal Post-Buckling and Aeroelastic Behavior of Shape Memory Alloy Reinforced Plates. Institute of Physics Publishing, Smart Material and Structure. Smart Mater. Struct. 11 (2002) 297-307, Apr. 5, 2002. http://www.wam.umd.edu/~mtawfik/sm2213.pdf.
    • (2002) Smart Mater. Struct. , vol.11 , pp. 297-307
    • Tawfik, M.1    Ro, J.2    Mei, C.3
  • 12
    • 18544399002 scopus 로고    scopus 로고
    • Flight test experience with an electromechanical actuator on the F-18 systems research aircraft
    • NASA Dryden Research Center, H-2425, October 7-13
    • Jensen, Steven C.; Jenney Gavin D.; Raymond, Bruce; Dawson, David.: Flight Test Experience With an Electromechanical Actuator on the F-18 Systems Research Aircraft. NASA Dryden Research Center, H-2425. 19th Digital Avionics Systems Conference, October 7-13, 2000.
    • (2000) 19th Digital Avionics Systems Conference
    • Jensen, S.C.1    Jenney Gavin, D.2    Raymond, B.3    Dawson, D.4
  • 20
    • 84885307083 scopus 로고
    • A conceptual framework for systems fault tolerance
    • March 30
    • A Conceptual Framework for Systems Fault Tolerance. Fault Tolerance Mechanisms. March 30, 1995. http://hissa.nist.gov/chissa/SEI_Framework/framework_16.htm 1
    • (1995) Fault Tolerance Mechanisms
  • 21
    • 84885310474 scopus 로고    scopus 로고
    • Department of Computer Science, University of York. York, England
    • Dawkins, Steven; McDermid, John: Defining an Acceptable Level of Redundancy. Department of Computer Science, University of York. York, England; 1998. http://www-users.cs.york.ac.uk/~steve/Published/TN-98-9.pdf
    • (1998) Defining an Acceptable Level of Redundancy
    • Dawkins, S.1    McDermid, J.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.