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Volumn 10, Issue , 2006, Pages 7006-7016

Actuation of an active Gurney flap for rotorcraft applications

Author keywords

[No Author keywords available]

Indexed keywords

CENTRIFUGAL (CF) LOADS; HIGH FREQUENCY ACTUATION; PIEZOELECTRIC BENDERS; ROTOR BLADES;

EID: 34247170450     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (20)

References (15)
  • 1
    • 30744465785 scopus 로고    scopus 로고
    • Miniature Trailing-Edge Effectors for Rotorcraft Applications,
    • M.S. Thesis, Department of Aerospace Engineering, Penn State University, University Park, PA
    • Kinzel, M.P., "Miniature Trailing-Edge Effectors for Rotorcraft Applications," M.S. Thesis, Department of Aerospace Engineering, Penn State University, University Park, PA, 2004.
    • (2004)
    • Kinzel, M.P.1
  • 2
    • 30744453544 scopus 로고    scopus 로고
    • Kinzel, M.P., Maughmer, M.D., Lesieutre, G.L., and Duque, E.P.N., Numerical Investigation of Miniature Trailing-Edge Effectors on Static and Oscillating Airfoils, AIAA Aerospace Sciences Meeting, Reno, NV, Jan. 10-13, 2005, AIAA 2005-1039.
    • Kinzel, M.P., Maughmer, M.D., Lesieutre, G.L., and Duque, E.P.N., "Numerical Investigation of Miniature Trailing-Edge Effectors on Static and Oscillating Airfoils," AIAA Aerospace Sciences Meeting, Reno, NV, Jan. 10-13, 2005, AIAA 2005-1039.
  • 4
    • 0031246730 scopus 로고    scopus 로고
    • Can a Coupling Coefficient of a Piezoelectric Actuator be Higher Than Those of Its Active Material?
    • Lesieutre, G.A., and C.L. Davis, "Can a Coupling Coefficient of a Piezoelectric Actuator be Higher Than Those of Its Active Material?," Journal of Intelligent Materials Systems and Structures, Vol. 8, 1997, pp. 859-867.
    • (1997) Journal of Intelligent Materials Systems and Structures , vol.8 , pp. 859-867
    • Lesieutre, G.A.1    Davis, C.L.2
  • 8
    • 0029215180 scopus 로고
    • Development of a piezoelectric servoflap for helicopter rotor control
    • Hall, S., Prechtl, E., "Development of a piezoelectric servoflap for helicopter rotor control," Active Materials and Smart Structures, Vol. 2427, 1995, pp. 16-29.
    • (1995) Active Materials and Smart Structures , vol.2427 , pp. 16-29
    • Hall, S.1    Prechtl, E.2
  • 9
    • 85003571577 scopus 로고
    • The Potential of Gurney Flaps for Improving the Aerodynamic Performance of Helicopter Rotors
    • AIAA Paper 93-4883
    • Kentfield, J.A.C., "The Potential of Gurney Flaps for Improving the Aerodynamic Performance of Helicopter Rotors," AIAA International Powered Lift Conference, pp. 283-292, AIAA Paper 93-4883, 1993.
    • (1993) AIAA International Powered Lift Conference , pp. 283-292
    • Kentfield, J.A.C.1
  • 11
    • 0033894883 scopus 로고    scopus 로고
    • Aerodynamics of Gurney Flaps on a Single-Element High-Lift Wing
    • March-April
    • Jeffrey, D., Zhang, X., Hurst, D.W., "Aerodynamics of Gurney Flaps on a Single-Element High-Lift Wing," Journal of Aircraft, Vol. 37, March-April 200, pp. 295-301.
    • Journal of Aircraft , vol.37 , Issue.200 , pp. 295-301
    • Jeffrey, D.1    Zhang, X.2    Hurst, D.W.3
  • 12
    • 84883544198 scopus 로고    scopus 로고
    • Design, Development, Fabrication and Testing of an Active Flap Rotor System
    • Grapevine, TX
    • Straub, F.K., Kennedy, D.K., "Design, Development, Fabrication and Testing of an Active Flap Rotor System," American Helicopter Society 61st Annual Forum, Grapevine, TX, 2005.
    • (2005) American Helicopter Society 61st Annual Forum
    • Straub, F.K.1    Kennedy, D.K.2
  • 13
    • 0035249554 scopus 로고    scopus 로고
    • Design of piezostack-driven trailing-edge flap actuator for helicopter rotors
    • Chopra, I., Lee, T., "Design of piezostack-driven trailing-edge flap actuator for helicopter rotors," Smart Materials and Structures, Vol. 10, 2001, pp. 15-21.
    • (2001) Smart Materials and Structures , vol.10 , pp. 15-21
    • Chopra, I.1    Lee, T.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.