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Volumn 1, Issue , 2003, Pages 151-156

Nonlinear dynamics and control of a wind-milling gyroplane rotor

Author keywords

Aerodynamics; Aircraft; Azimuth; Blades; Fasteners; Helicopters; Mechanical systems; Milling; Production; Stability

Indexed keywords

AERODYNAMIC STABILITY; AERODYNAMICS; AIRCRAFT; CONVERGENCE OF NUMERICAL METHODS; FASTENERS; HELICOPTERS; PRODUCTION;

EID: 34247113936     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/PHYCON.2003.1236805     Document Type: Conference Paper
Times cited : (9)

References (12)
  • 1
    • 0004245020 scopus 로고
    • Mir, (A Russian translation)
    • W. Johnson, Helicopter Theory, vol. 1, Mir, 1983. (A Russian translation).
    • (1983) Helicopter Theory , vol.1
    • Johnson, W.1
  • 3
    • 84945416364 scopus 로고    scopus 로고
    • A computational model for rotor-fuselage interactional aerodynamics
    • D.D. Boyd, R.W. Barnwell, and S.A. Gorton, "A computational model for rotor-fuselage interactional aerodynamics," AIAA Paper, no. 0256, pp. 1-10, 2002.
    • (2002) AIAA Paper, No. 0256 , pp. 1-10
    • Boyd, D.D.1    Barnwell, R.W.2    Gorton, S.A.3
  • 5
    • 84945327168 scopus 로고    scopus 로고
    • The Irkutsk's gyroplane
    • Russian
    • O.Ye. Polyntsev and A.A. Kalmykov, "The Irkutsk's gyroplane," Vertolet, no. 3, pp. 20-22, 2000. (Russian).
    • (2000) Vertolet , Issue.3 , pp. 20-22
    • Polyntsev, O.Ye.1    Kalmykov, A.A.2
  • 10
    • 10444254498 scopus 로고
    • Computation of the stress' into a helicopter's main rotor blade at a large flight speed
    • Russian
    • A.V. Nekrasov, "Computation of the stress' into a helicopter's main rotor blade at a large flight speed," Proceedings of the TsAGI, no. 898, pp. 40-71, 1964. (Russian).
    • (1964) Proceedings of the TsAGI , Issue.898 , pp. 40-71
    • Nekrasov, A.V.1
  • 12
    • 33644786055 scopus 로고    scopus 로고
    • Robust stabilization of a flexible spacecraft at partial discrete measurement and a delay in forming control
    • Ye.I. Somov, "Robust stabilization of a flexible spacecraft at partial discrete measurement and a delay in forming control," Journal of Computer and Systems Sciences International, vol. 40, no. 2, pp. 287-307, 2001.
    • (2001) Journal of Computer and Systems Sciences International , vol.40 , Issue.2 , pp. 287-307
    • Somov, Ye.I.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.