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Volumn 40, Issue 6, 2003, Pages 1123-1130

Calculation of rotor blade-vortex interaction airloads using a multiple-trailer free-wake model

Author keywords

[No Author keywords available]

Indexed keywords

FLOW INTERACTIONS; HELICOPTER ROTORS; MATHEMATICAL MODELS; VORTEX FLOW; WAKES;

EID: 0346503130     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.7200     Document Type: Article
Times cited : (47)

References (20)
  • 12
    • 0031190234 scopus 로고    scopus 로고
    • Blade-vortex interaction noise prediction using a rotor wake rollup model
    • Rahier, G., and Delrieux, Y., "Blade-Vortex Interaction Noise Prediction Using a Rotor Wake Rollup Model," Journal of Aircraft, Vol. 34, No. 4, 1997, pp. 522-530.
    • (1997) Journal of Aircraft , vol.34 , Issue.4 , pp. 522-530
    • Rahier, G.1    Delrieux, Y.2
  • 14
    • 0346924170 scopus 로고    scopus 로고
    • Prediction of blade-vortex interaction airloads with higher-harmonic pitch controls using the 2GCHAS comprehensive code
    • Lim, J. W., Tung, C., and Yu, Y. H., "Prediction of Blade-Vortex Interaction Airloads with Higher-Harmonic Pitch Controls Using the 2GCHAS Comprehensive Code," Journal of Pressure Vessel Technology, Vol. 123, No. 4, 2001, pp. 469-474.
    • (2001) Journal of Pressure Vessel Technology , vol.123 , Issue.4 , pp. 469-474
    • Lim, J.W.1    Tung, C.2    Yu, Y.H.3
  • 18
    • 0003677643 scopus 로고
    • Computation of helicopter rotor wake geometry and its influence on rotor harmonic airloads
    • Aeroelastic and Structures Research Lab., Dept. of Aeronautics and Astronautics, Massachusetts Inst. of Technology, ASRL TR 178-1, Cambridge, MA, March
    • Scully, M. P., "Computation of Helicopter Rotor Wake Geometry and its Influence on Rotor Harmonic Airloads," Aeroelastic and Structures Research Lab., Dept. of Aeronautics and Astronautics, Massachusetts Inst. of Technology, ASRL TR 178-1, Cambridge, MA, March 1975.
    • (1975)
    • Scully, M.P.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.