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Volumn 2, Issue , 2005, Pages 2057-2075

Implementation of a free-vortex wake model in real-time simulation of rotorcraft

Author keywords

[No Author keywords available]

Indexed keywords

FINITE-STATE INFLOW MODELS; FREE-VORTEX WAKE MODELS; REAL-TIME SIMULATION; ROLL AXES;

EID: 33644672067     PISSN: 15522938     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (5)

References (15)
  • 4
    • 4243512305 scopus 로고
    • Influence of dynamic inflow on the helicopter vertical response
    • Chen, R. T. N., and Hindson, W. S., "Influence of Dynamic Inflow on the Helicopter Vertical Response," Vertica, Vol. 11, No. 1, pp. 77-91, 1989.
    • (1989) Vertica , vol.11 , Issue.1 , pp. 77-91
    • Chen, R.T.N.1    Hindson, W.S.2
  • 5
    • 0003753630 scopus 로고
    • A survey of nonuniform inflow models for rotorcraft flight dynamics and control applications
    • Chen, R. T. N., "A Survey of Nonuniform Inflow Models for Rotorcraft Flight Dynamics and Control Applications," Vertica, Vol. 14, No. 2, pp. 147-184, 1990.
    • (1990) Vertica , vol.14 , Issue.2 , pp. 147-184
    • Chen, R.T.N.1
  • 6
    • 23844515893 scopus 로고
    • UH-60A BLACK HAWK engineering simulation program: Volume I - Mathematical model
    • USAAVSCOM TR 89-A-001, September
    • Hewlett, J., "UH-60A BLACK HAWK Engineering Simulation Program: Volume I - Mathematical Model", NASA CR-177542, USAAVSCOM TR 89-A-001, September 1989.
    • (1989) NASA CR-177542
    • Hewlett, J.1
  • 14
    • 84888776508 scopus 로고    scopus 로고
    • High fidelity helicopter simulation using free wake, lifting line tail, and blade element tail rotor models
    • Phoenix, AZ, May
    • th Annual Forum, Phoenix, AZ, May 2003.
    • (2003) th Annual Forum
    • Spoldi, S.1    Ruckel, P.2
  • 15
    • 0026889693 scopus 로고
    • Frequency-response methods for rotorcraft system identification: Flight applications to BO-105 coupled rotor/fuselage dynamics
    • July
    • Tischler, M.B., and Cauffman, M.G., "Frequency-Response Methods for Rotorcraft System Identification: Flight Applications to BO-105 Coupled Rotor/Fuselage Dynamics," Journal of the American Helicopter Society, Vol. 37, No. 3, pp. 3-17, July 1992.
    • (1992) Journal of the American Helicopter Society , vol.37 , Issue.3 , pp. 3-17
    • Tischler, M.B.1    Cauffman, M.G.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.