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Volumn 3327, Issue , 1998, Pages 73-84

Aeromechanical stability augmentation of helicopters using Enhanced Active Constrained Layer (EACL) treatment on flex beams

Author keywords

Active passive hybrid control; Adaptive flex beam; Enhanced active constrained layer damping; Rotor stability augmentation

Indexed keywords

ACTUATORS; BEAMS AND GIRDERS; ELECTRIC FIELD EFFECTS; FINITE ELEMENT METHOD; HELICOPTER ROTORS; MATHEMATICAL MODELS; STIFFNESS;

EID: 0032403554     PISSN: 0277786X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1117/12.310714     Document Type: Conference Paper
Times cited : (4)

References (25)
  • 1
    • 0001330496 scopus 로고
    • Perspectives in aeromechanical stability of helicopter rotors
    • (1990) Vertica , vol.14 , Issue.4
    • Chopra, I.1
  • 7
    • 0010358816 scopus 로고
    • Optimal control of helicopter aeromechanical stability
    • (1987) Vertica , vol.11 , Issue.3 , pp. 425-435
    • Straub, F.K.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.