메뉴 건너뛰기




Volumn 44, Issue 3, 2007, Pages 936-944

Simplified rotor inflow model for descent flight

Author keywords

[No Author keywords available]

Indexed keywords

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

EID: 34547173652     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.25910     Document Type: Article
Times cited : (6)

References (29)
  • 1
    • 0003340216 scopus 로고
    • Empirical Relation Between Induced Velocity, Thrust, and Rate of Descent of a Helicopter Rotor as Determined by Wind Tunnel Tests on Four Model Rotors
    • Oct
    • Castles, W., Jr., and Gray, R. B., "Empirical Relation Between Induced Velocity, Thrust, and Rate of Descent of a Helicopter Rotor as Determined by Wind Tunnel Tests on Four Model Rotors," NACA TN 2474, Oct. 1951.
    • (1951) NACA TN , vol.2474
    • Castles Jr., W.1    Gray, R.B.2
  • 2
    • 0012757396 scopus 로고
    • Wind Tunnel Tests of Two VTOL Propellers in Descent
    • March
    • Yaggy, P. F., and Mort, K. W., "Wind Tunnel Tests of Two VTOL Propellers in Descent," NACA TN D-1766, March 1963.
    • (1963) NACA TN , vol.D-1766
    • Yaggy, P.F.1    Mort, K.W.2
  • 3
    • 85003253284 scopus 로고
    • Experiments on a Model Helicopter Rotor Operating in the Vortex Ring State
    • May-June
    • Washizu, K., Azuma, A., Koo, J., and Oka, T., "Experiments on a Model Helicopter Rotor Operating in the Vortex Ring State," Journal of Aircraft, Vol. 3, No. 3, May-June 1966, pp. 225-230.
    • (1966) Journal of Aircraft , vol.3 , Issue.3 , pp. 225-230
    • Washizu, K.1    Azuma, A.2    Koo, J.3    Oka, T.4
  • 4
    • 4143094707 scopus 로고
    • Analytic Prediction of Vortex-Ring Boundaries for Helicopters in Steep Descents
    • July
    • Wolkovitch, J., "Analytic Prediction of Vortex-Ring Boundaries for Helicopters in Steep Descents," Journal of the American Helicopter Society, Vol. 17, No. 3, July 1971, pp. 13-19.
    • (1971) Journal of the American Helicopter Society , vol.17 , Issue.3 , pp. 13-19
    • Wolkovitch, J.1
  • 5
    • 85003338364 scopus 로고
    • Induced Flow Variation of the Helicopter Rotor Operating in the Vortex Ring State
    • July-Aug
    • Azuma, A., and Obata, A., "Induced Flow Variation of the Helicopter Rotor Operating in the Vortex Ring State," Journal of Aircraft, Vol. 5, No. 4, July-Aug. 1968, pp. 381-386.
    • (1968) Journal of Aircraft , vol.5 , Issue.4 , pp. 381-386
    • Azuma, A.1    Obata, A.2
  • 6
    • 85069345449 scopus 로고
    • Tail-Rotor Thrust on a 5.5-foot Helicopter Model in Ground Effect
    • American Helicopter Society, Washington, D.C, May
    • Empey, R. W., and Ormiston, R. A., "Tail-Rotor Thrust on a 5.5-foot Helicopter Model in Ground Effect," American Helicopter Society Annual National Forum, American Helicopter Society, Washington, D.C., May 1974.
    • (1974) American Helicopter Society Annual National Forum
    • Empey, R.W.1    Ormiston, R.A.2
  • 7
    • 0025232923 scopus 로고
    • Analytical Approach to the Induced Flow of a Helicopter Rotor in Vertical Descent
    • Jan
    • Wang, S. C., "Analytical Approach to the Induced Flow of a Helicopter Rotor in Vertical Descent," Journal of the American Helicopter Society, Vol. 35, Jan. 1990, pp. 92-98.
    • (1990) Journal of the American Helicopter Society , vol.35 , pp. 92-98
    • Wang, S.C.1
  • 8
    • 29244476836 scopus 로고
    • Experimental Investigation of Model Rotors Operating in Vertical Descent
    • Sept
    • Xin, H., and Gao, Z., "Experimental Investigation of Model Rotors Operating in Vertical Descent," 19th European Rotorcraft Forum, Sept. 1993.
    • (1993) 19th European Rotorcraft Forum
    • Xin, H.1    Gao, Z.2
  • 16
    • 34547188500 scopus 로고    scopus 로고
    • Glauert, H., Analysis of Experimental Results in the Windmill Bake and Vortex Ring States of an Airscrew, R. & M. No. 1026, British Aeronautical Research Council, 1926.
    • Glauert, H., "Analysis of Experimental Results in the Windmill Bake and Vortex Ring States of an Airscrew," R. & M. No. 1026, British Aeronautical Research Council, 1926.
  • 17
    • 0034296214 scopus 로고    scopus 로고
    • Finite State Induced Flow Model in Vortex Ring State
    • Oct
    • He, C. J., Lee, C. S., Chen, W. B., "Finite State Induced Flow Model in Vortex Ring State," Journal of the American Helicopter Society, Vol. 45, No. 4, Oct. 2000, pp. 318-320.
    • (2000) Journal of the American Helicopter Society , vol.45 , Issue.4 , pp. 318-320
    • He, C.J.1    Lee, C.S.2    Chen, W.B.3
  • 19
    • 4143138579 scopus 로고
    • Momentum Theory, Dynamic Inflow, and the Vortex Ring State
    • July
    • Peters, D. A., and Chen, S. Y., "Momentum Theory, Dynamic Inflow, and the Vortex Ring State," Journal of the American Helicopter Society, Vol. 28, No. 3, July 1982, pp. 18-24.
    • (1982) Journal of the American Helicopter Society , vol.28 , Issue.3 , pp. 18-24
    • Peters, D.A.1    Chen, S.Y.2
  • 20
    • 0004245020 scopus 로고
    • Princeton Univ. Press, Princeton, NJ
    • Johnson, W., Helicopter Theory, Princeton Univ. Press, Princeton, NJ, 1980, pp. 98-102.
    • (1980) Helicopter Theory , pp. 98-102
    • Johnson, W.1
  • 22
    • 4143049026 scopus 로고
    • The Normal Component of the Induced Velocity in the Vicinity of a Lifting Rotor and Some Examples of its Application
    • Castles, W., and Leeuw, J. H., "The Normal Component of the Induced Velocity in the Vicinity of a Lifting Rotor and Some Examples of its Application," NACA TN 2912, 1953.
    • (1953) NACA TN , vol.2912
    • Castles, W.1    Leeuw, J.H.2
  • 27
    • 0003642117 scopus 로고
    • Development and Application of a Generalized Dynamic Wake Theory for Lifting Rotors,
    • Ph.D. Dissertation, Georgia Inst. of Technology, School of Aerospace Engineering, Aug
    • He, C. J., "Development and Application of a Generalized Dynamic Wake Theory for Lifting Rotors," Ph.D. Dissertation, Georgia Inst. of Technology, School of Aerospace Engineering, Aug. 1989.
    • (1989)
    • He, C.J.1
  • 28
    • 2942589003 scopus 로고
    • Momentum Analysis of Helicopters and Autogyros in Inclined Descent, with Comments on Operational Restrictions
    • Oct
    • Heyson, H. H., "Momentum Analysis of Helicopters and Autogyros in Inclined Descent, with Comments on Operational Restrictions," NASA TN D-7917, Oct. 1975.
    • (1975) NASA TN , vol.D-7917
    • Heyson, H.H.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.