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Volumn 40, Issue 9, 2002, Pages 1717-1725

Forward flight stability characteristics for composite hingeless rotors with transverse shear deformation

Author keywords

[No Author keywords available]

Indexed keywords

ANISOTROPY; COMPOSITE MATERIALS; COMPRESSIBILITY; COMPUTER SIMULATION; EQUATIONS OF MOTION; FINITE ELEMENT METHOD; FLIGHT DYNAMICS; SHAFTS (MACHINE COMPONENTS); SHEAR DEFORMATION; TORSIONAL STRESS;

EID: 0036715067     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1875     Document Type: Article
Times cited : (8)

References (32)
  • 9
    • 0003284358 scopus 로고
    • An experimental investigation of the flap-lag-torsion aeroelastic stability of a small-scale hingeless helicopter rotor in hover
    • Jan.
    • (1986) NASA TP , vol.2546
    • Sharpe, D.L.1
  • 10
    • 0025548966 scopus 로고
    • Helicopter rotor dynamics and aeroelasticity: Some key ideas and insights
    • (1990) Vertica , vol.14 , Issue.1 , pp. 101-121
    • Friedmann, P.P.1
  • 12
  • 16
    • 0028413864 scopus 로고
    • Aeroelastic response of composite rotor blades considering transverse shear and structural damping
    • (1994) AIAA Journal , vol.32 , Issue.4 , pp. 820-827
    • Jung, S.N.1    Kim, S.J.2
  • 17
    • 0029357794 scopus 로고
    • Effect of transverse shear on aeroelastic stability of a composite rotor blade
    • (1995) AIAA Journal , vol.33 , Issue.8 , pp. 1541-1543
    • Jung, S.N.1    Kim, S.J.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.