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Volumn 110, Issue 1114, 2006, Pages 793-801

Aeroelastic response of helicopter rotors using a 3D unsteady aerodynamic solver

Author keywords

[No Author keywords available]

Indexed keywords

HELICOPTERS; MATHEMATICAL MODELS; THREE DIMENSIONAL; TURBOMACHINE BLADES; VORTEX FLOW;

EID: 34250214598     PISSN: 00019240     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0001924000001664     Document Type: Article
Times cited : (37)

References (24)
  • 1
    • 0346503130 scopus 로고    scopus 로고
    • Calculation of rotor bladevortex interaction airloads using a multiple-trailer free-wake model
    • LIM, J.W., YU, Y.H. and JOHNSON, W. Calculation of rotor bladevortex interaction airloads using a multiple-trailer free-wake model, J Aircr 2003, 40, (6), pp 1123-1130.
    • (2003) J Aircr , vol.40 , Issue.6 , pp. 1123-1130
    • LIM, J.W.1    YU, Y.H.2    JOHNSON, W.3
  • 2
    • 22544476993 scopus 로고    scopus 로고
    • An analysis of helicopter blade-vortex interaction noise with flight path or attitude modification
    • Montreal, Canada
    • MUNSKY, B., GANDHI, F. and TAUSZIG, L. An analysis of helicopter blade-vortex interaction noise with flight path or attitude modification, 58th Annual Forum of the American Helicopter Society, 2002, Montreal, Canada.
    • (2002) 58th Annual Forum of the American Helicopter Society
    • MUNSKY, B.1    GANDHI, F.2    TAUSZIG, L.3
  • 3
  • 4
    • 14144249428 scopus 로고    scopus 로고
    • Rotorcraft vibration reduction and noise predictions using a unified aeroelastic response simulation
    • PATT, D., LIU, L. and FRIEDMANN, P.P. Rotorcraft vibration reduction and noise predictions using a unified aeroelastic response simulation, J American Helicopter Society, 2005, 50, (1), pp 95-106.
    • (2005) J American Helicopter Society , vol.50 , Issue.1 , pp. 95-106
    • PATT, D.1    LIU, L.2    FRIEDMANN, P.P.3
  • 5
    • 27544471888 scopus 로고    scopus 로고
    • Description and validation of the ONERA computational methods for the prediction of blade-vortex interaction noise
    • BEAUMIER, P. and DELRIEUX, Y. Description and validation of the ONERA computational methods for the prediction of blade-vortex interaction noise, Aerospace Science and Technology, 2005, 9, pp 31-43.
    • (2005) Aerospace Science and Technology , vol.9 , pp. 31-43
    • BEAUMIER, P.1    DELRIEUX, Y.2
  • 6
    • 4344645668 scopus 로고    scopus 로고
    • Validation and understanding of UH-60A vibratory loads in steady level flight
    • DATTA, A. and CHOPRA, I. Validation and understanding of UH-60A vibratory loads in steady level flight, J American Helicopter Society, 2004, 49, (3), pp 271-287.
    • (2004) J American Helicopter Society , vol.49 , Issue.3 , pp. 271-287
    • DATTA, A.1    CHOPRA, I.2
  • 7
    • 0031685894 scopus 로고    scopus 로고
    • Dynamics workshop on rotor vibratory loads prediction
    • HANSFORD, R.E. and VORWALD, J. Dynamics workshop on rotor vibratory loads prediction, J American Helicopter Society, 1998, 31, (1), pp 76-87.
    • (1998) J American Helicopter Society , vol.31 , Issue.1 , pp. 76-87
    • HANSFORD, R.E.1    VORWALD, J.2
  • 8
    • 0004090333 scopus 로고
    • Nonlinear equation for the elastic bending and torsion of twisted nonuniform rotor blades
    • HODGES, D.H. and DOWELL, E.H. Nonlinear equation for the elastic bending and torsion of twisted nonuniform rotor blades, NASA TN D7818, 1974.
    • (1974) NASA TN , vol.D7818
    • HODGES, D.H.1    DOWELL, E.H.2
  • 10
    • 84977134611 scopus 로고    scopus 로고
    • Coupled free-wakeaerodynamics/blade-dynamics analyses of rotors in forward flight
    • AIAA Paper 98-2241, Toulouse, France
    • GENNARETTI, M., CORSETTI, E. and MORINO, L. Coupled free-wakeaerodynamics/blade-dynamics analyses of rotors in forward flight, AIAA Paper 98-2241, 4th AIAA/CEAS Aeroacoustic Conference, May 1998, Toulouse, France.
    • (1998) 4th AIAA/CEAS Aeroacoustic Conference, May
    • GENNARETTI, M.1    CORSETTI, E.2    MORINO, L.3
  • 11
    • 29244433221 scopus 로고    scopus 로고
    • A novel potential-flow boundary integral formulation for helicopter rotors in BVI conditions
    • AIAA Paper 2005-2924, Monterey, California, USA
    • GENNARETTI, M. and BERNARDINI, G. A novel potential-flow boundary integral formulation for helicopter rotors in BVI conditions, AIAA Paper 2005-2924, 11th AIAA/CEAS Aeroacoustic Conference, May 2005, Monterey, California, USA.
    • (2005) 11th AIAA/CEAS Aeroacoustic Conference, May
    • GENNARETTI, M.1    BERNARDINI, G.2
  • 13
    • 2942616925 scopus 로고
    • Stability of elastic bending and torsion of uniform cantilever rotor blades in hover with variable structural coupling
    • HODGES, D.H. and ORMISTON R.A. Stability of elastic bending and torsion of uniform cantilever rotor blades in hover with variable structural coupling, NASA TN D-8192, 1976.
    • (1976) NASA TN , vol.D-8192
    • HODGES, D.H.1    ORMISTON, R.A.2
  • 14
    • 0022195251 scopus 로고
    • Free wake analysis of helicopter rotors
    • MORINO, L., KAPRIELIAN, Z., JR. and SIPCIC, S.R. Free wake analysis of helicopter rotors, Vertica, 1985, 9, (2), pp 127-140.
    • (1985) Vertica , vol.9 , Issue.2 , pp. 127-140
    • MORINO, L.1    KAPRIELIAN, Z.J.2    SIPCIC, S.R.3
  • 16
    • 0003927402 scopus 로고    scopus 로고
    • General theory of aerodynamic instability and the mechanism of flutter
    • 496, 1935
    • THEODORSEN, T. General theory of aerodynamic instability and the mechanism of flutter, NACA Report 496, 1935.
    • NACA Report
    • THEODORSEN, T.1
  • 17
    • 0039644938 scopus 로고
    • A theory of airflow through rotors and its application to some helicopter problems
    • DREES, J.M. A theory of airflow through rotors and its application to some helicopter problems, J Helicopter Association of Great Britain, 1949, 3, (2), pp 79-104.
    • (1949) J Helicopter Association of Great Britain , vol.3 , Issue.2 , pp. 79-104
    • DREES, J.M.1
  • 19
    • 85039181023 scopus 로고    scopus 로고
    • BIR, G. and CHOPRA, I., et al. University of Maryland advanced rotor code (UMARC) Theory Manual, Technical Report UM-AERO 94-18, Center for Rotorcraft Education and Research, University of Maryland, College Park, 1994, Maryland, USA.
    • BIR, G. and CHOPRA, I., et al. University of Maryland advanced rotor code (UMARC) Theory Manual, Technical Report UM-AERO 94-18, Center for Rotorcraft Education and Research, University of Maryland, College Park, 1994, Maryland, USA.
  • 20
    • 0043219992 scopus 로고
    • Boundary integral equation methods for aerodynamics, computational nonlinear mechanics in aerospace engineering
    • edited by ATLURI, S.N, AIAA, Washington, DC, USA, pp
    • MORINO, L. and GENNARETTI, M. Boundary integral equation methods for aerodynamics, computational nonlinear mechanics in aerospace engineering, edited by ATLURI, S.N. Progress in Aeronautics & Astronautics, 1992, 146, AIAA, Washington, DC, USA, pp 279-320.
    • (1992) Progress in Aeronautics & Astronautics , vol.146 , pp. 279-320
    • MORINO, L.1    GENNARETTI, M.2
  • 21
    • 0031555839 scopus 로고    scopus 로고
    • A unified boundary integral methodology for aerodynamics and aeroacoustics of rotors
    • GENNARETTI, M., LUCERI, L., and MORINO, L. A unified boundary integral methodology for aerodynamics and aeroacoustics of rotors, J Sound and Vibrations, 1997, 200, (4), pp 467-489.
    • (1997) J Sound and Vibrations , vol.200 , Issue.4 , pp. 467-489
    • GENNARETTI, M.1    LUCERI, L.2    MORINO, L.3
  • 24
    • 85039218323 scopus 로고    scopus 로고
    • LIM, J.W., TUNG, C., YU, Y.H., BURLEY, C.L., BROOKS, T., BOYD, D., VAN DER WALL, B., SCHNEIDER, O., RICHARD, H., RAFFEL, M., BEAUMIER, P., BAILLY, J., DELRIEUX, Y., PENGEL, K. and MERCKER, E. HART II: Prediction of blade-vortex interaction loading, 29th European Rotorcraft Forum, September 2003, Friedrichshafen, Germany.
    • LIM, J.W., TUNG, C., YU, Y.H., BURLEY, C.L., BROOKS, T., BOYD, D., VAN DER WALL, B., SCHNEIDER, O., RICHARD, H., RAFFEL, M., BEAUMIER, P., BAILLY, J., DELRIEUX, Y., PENGEL, K. and MERCKER, E. HART II: Prediction of blade-vortex interaction loading, 29th European Rotorcraft Forum, September 2003, Friedrichshafen, Germany.


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.