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Volumn 47, Issue 2, 2002, Pages 123-133

Vibratory loads reduction testing of the NASA/Army/MIT active twist rotor

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; PIEZOELECTRICITY; PRODUCT DESIGN; TURBOMACHINE BLADES; VIBRATION CONTROL; WIND TUNNELS;

EID: 0036538117     PISSN: 00028711     EISSN: None     Source Type: Journal    
DOI: 10.4050/jahs.47.123     Document Type: Article
Times cited : (102)

References (22)
  • 14
    • 0004026687 scopus 로고    scopus 로고
    • Development of an integral twist-actuated rotor blade for individual blade control
    • Active Materials and Structures Laboratory, Massachusetts Institute of Technology, October
    • (1998) AMSL Report , vol.98 , Issue.6
    • Rodgers, J.P.1    Hagood, N.W.2
  • 17
    • 0005849945 scopus 로고    scopus 로고
    • Design, manufacturing and testing of an active twist rotor
    • Active Materials and Structures Laboratory, Massachusetts Institute of Technology, June
    • (1999) AMSL Report , vol.99 , Issue.3
    • Shin, S.1    Cesnik, C.E.S.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.