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Volumn 2, Issue , 2011, Pages 1079-1104

Design, evaluation and test of active trailing edge

Author keywords

[No Author keywords available]

Indexed keywords

ACTIVE ROTOR; BLADE DEFORMATION; CROSS SECTION; CURING PROCESS; FULL SCALE TESTS; MORPHING; PIEZOCERAMIC; ROTOR BLADES; TRAILING EDGE FLAPS; TRAILING EDGES; VIBRATION REDUCTIONS;

EID: 79960687153     PISSN: 15522938     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (9)

References (25)
  • 8
    • 79960675190 scopus 로고
    • Results of the 1986 NASA/FAA/DFVLR main rotor test entry in the German-Dutch wind runnel (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 runnel (DNW)," NASA Technical Memorandum 100507, October 1987.
    • (1987) NASA Technical Memorandum 100507
    • Brooks, T.F.1    Martin, R.M.2
  • 11
    • 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    Byrns Jr., E.V.2
  • 24
    • 79960661425 scopus 로고    scopus 로고
    • www.bluecopter.com


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.