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Volumn 46, Issue 4, 2001, Pages 290-300

Multibody modeling of engage and disengage operations of helicopter rotors

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; DEFORMATION; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; TURBOMACHINE BLADES;

EID: 0035482073     PISSN: 00028711     EISSN: None     Source Type: Journal    
DOI: 10.4050/jahs.46.290     Document Type: Article
Times cited : (33)

References (34)
  • 1
    • 0006543488 scopus 로고
    • Wind tunnel measurements of ship induced turbulence and the prediction of helicopter rotor blade response
    • (1988) Vertica , vol.12 , pp. 267-278
    • Hurst, D.W.1    Newman, S.J.2
  • 2
    • 0006529775 scopus 로고
    • A theoretical model for predicting the blade sailing behaviour of a semi-rigid rotor helicopter
    • (1990) Vertica , vol.14 , pp. 531-544
    • Newman, S.J.1
  • 6
    • 0003558929 scopus 로고
    • Aeroelastic analysis of transient blade dynamics during shipboard engage/disengage operations
    • Master's Thesis, Pennsylvania State University
    • (1995)
    • Geyer W.P., Jr.1
  • 10
    • 0004091291 scopus 로고
    • Differential equations of motion for combined flapwise bending, chordwise bending, and torsion of twisted nonuniform rotor blades
    • Technical Report 1348, NACA Report
    • (1958)
    • Houbolt, J.C.1    Brooks, G.W.2
  • 11
    • 0004090333 scopus 로고
    • Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades
    • Technical Report, NASA TN D-7818
    • (1974)
    • Hodges, D.H.1    Dowell, E.H.2
  • 32
    • 0003617551 scopus 로고    scopus 로고
    • An experimental and theoretical correlation of an analysis for helicopter rotor blade and droop stop impacts
    • Master's Thesis, Pennsylvania State University
    • (1997)
    • Keller, J.A.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.