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Volumn 2005, Issue , 2005, Pages

Rotorcraft simulation modelling and validation for control design and load prediction

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; DEGREES OF FREEDOM (MECHANICS); FLIGHT DYNAMICS; LOADS (FORCES); MATHEMATICAL MODELS;

EID: 33746617546     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (7)

References (25)
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    • Padfield, G.D.1    White, M.D.2
  • 2
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    • The NRC bell 412 advanced system research aircraft - A new facility for airborne simulation
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    • Gubbels, A.W., Carignan, S.J.R.P., "The NRC Bell 412 Advanced System Research Aircraft - A New Facility for Airborne Simulation", Canadian Aeronautics and Space Journal, Vol 46, No. 2, Jun, 2000, p106-115.
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  • 6
    • 0029276936 scopus 로고
    • Finite state induced flow models part II: Three dimensional rotor disk
    • March-April
    • Peters, D. A. and He, Chengjian, "Finite State Induced Flow Models Part II: Three dimensional Rotor Disk", Journal of Aircraft, Vol. 32, No. 2, March-April 1995.
    • (1995) Journal of Aircraft , vol.32 , Issue.2
    • Peters, D.A.1    He, C.2
  • 9
    • 58149501549 scopus 로고
    • Aerodynamic characteristics of two rotorcraft airfoils designed for application to inboard region of a main rotor blade
    • July
    • Noonan, K. W., "Aerodynamic Characteristics of Two Rotorcraft Airfoils Designed for Application to Inboard Region of a Main Rotor Blade", NASATP-3009, July 1990.
    • (1990) NASATP-3009
    • Noonan, K.W.1
  • 10
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    • Dadone, L.U.1
  • 11
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    • A method of computing helicopter vortex wake distortion
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    • Scully, M.P.1
  • 13
    • 0003663515 scopus 로고
    • Wake model for helicopter in high speed flight
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    • Johnson, W., "Wake Model for Helicopter in High Speed Flight", NASA CR- CR-1177507, Nov. 1988
    • (1988) NASA CR- CR-1177507
    • Johnson, W.1
  • 14
    • 34047268611 scopus 로고
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  • 16
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  • 17
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    • Wind-tunnel investigation of helicopter-rotor wake effects on three helicopter fuselage models
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    • Wilson, J.C.1    Mineck, R.E.2
  • 18
  • 20
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  • 23
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  • 24
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    • Rotorcraft simulation model enhancement to support design, testing and operational analysis
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.