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Volumn 39, Issue 4, 2002, Pages 668-677

Helicopter vibration reduction using discrete controllable-stiffness devices at the rotor hub

Author keywords

[No Author keywords available]

Indexed keywords

DRAG; OPTIMIZATION; STIFFNESS; TORSIONAL STRESS; VIBRATIONS (MECHANICAL);

EID: 0036651030     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2980     Document Type: Article
Times cited : (4)

References (27)
  • 1
    • 0019701953 scopus 로고
    • Helicopter vibration control-survey
    • (1981) Vertica , vol.5 , Issue.1 , pp. 1-20
    • Reichert, G.1
  • 17
    • 0003270161 scopus 로고
    • Comparison of analytical and experimental results for a semi-active vibration isolator
    • The Shock and Vibration Information Center, Naval Research Lab., Washington, DC
    • (1980) The Shock and Vibration Bulletin , vol.50 , Issue.PART 4 , pp. 69-76
    • Krasnicki, E.J.1
  • 18
    • 0021442183 scopus 로고
    • The experimental performance of an off-road vehicle utilizing a semi-active suspension
    • The Shock and Vibration Information Center, Naval Research Lab., Washington, DC
    • (1984) The Shock and Vibration Bulletin , vol.54 , Issue.PART 3 , pp. 135-142
    • Krasnicki, E.J.1
  • 24
    • 0012471984 scopus 로고
    • University of maryland advanced rotorcraft code (UMARC) theory manual
    • Univ. of Maryland, College Park, MD, Aug.
    • (1992) UM-AERO Rept. , vol.92 , Issue.2
    • Bir, G.1    Chopra, I.2
  • 27
    • 0003225607 scopus 로고
    • Self-tuning regulators for multicyclic control of helicopter vibration
    • March
    • (1982) NASA TP , vol.1996
    • Johnson, W.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.