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Volumn 2, Issue , 2007, Pages 923-961

Actuator design for the active trailing edge of a helicopter rotor blade

Author keywords

Adaptive helicopter rotor blade; Aero servo elasticity; Electro active composite; IBC actuator; Piezo ceramics; Smart materials

Indexed keywords

ACTIVE COMPOSITES; ADAPTIVE HELICOPTER ROTOR BLADE; ELECTRO-ACTIVE COMPOSITE; HELICOPTER ROTOR BLADES; PIEZO-CERAMICS; SMART MATERIALS;

EID: 77954231502     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (14)

References (36)
  • 1
    • 79960675190 scopus 로고
    • Results of the 1986 NASA/FAA/DFVLR main rotor test entry in the German-Dutch wind tunnel (DNW)
    • October
    • Brooks, T. F. and Martin, R. M., "Results of the 1986 NASA/FAA/DFVLR main rotor test entry in the German-Dutch wind tunnel (DNW)," NASA Technical Memorandum 100507, October 1987.
    • (1987) NASA Technical Memorandum 100507
    • Brooks, T.F.1    Martin, R.M.2
  • 4
    • 0022990667 scopus 로고
    • Application of Higher Harmonic Blade Feathering on the OH-6A Helicopter for Vibration Reduction
    • December
    • Straub, F. K. and E.V. Byrns, J., "Application of Higher Harmonic Blade Feathering on the OH-6A Helicopter for Vibration Reduction," NASA Contractor Report 4031, December 1986.
    • (1986) NASA Contractor Report 4031
    • Straub, F.K.1    EV Byrns, J.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.