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Volumn 9, Issue , 2005, Pages 5832-5846

Smart spring control of vibration and noise in helicopter blades

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC VARIABLES CONTROL; HELICOPTERS; MATHEMATICAL MODELS; STRUCTURAL LOADS; TURBOMACHINE BLADES;

EID: 28844496761     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-2270     Document Type: Conference Paper
Times cited : (6)

References (21)
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    • Vertica , vol.14 , pp. 3-22
    • Kretz, M.1    Larche, M.2
  • 2
    • 0343559156 scopus 로고
    • Can smart materials modify the blade root boundary conditions to attenuate helicopter vibration?
    • Technomic Publishing Co.
    • Nitzsche, F., Lammering, R. and Breitbach, E., "Can Smart Materials Modify the Blade Root Boundary Conditions to Attenuate Helicopter Vibration?" in the Fourth International Conference on Adaptive Structures, Technomic Publishing Co., 1994, pp.139-150.
    • (1994) Fourth International Conference on Adaptive Structures , pp. 139-150
    • Nitzsche, F.1    Lammering, R.2    Breitbach, E.3
  • 3
    • 28844501161 scopus 로고    scopus 로고
    • (inventors). Structural Component Having Means for Actively Varying its Stiffness to Control Vibrations, U.S. Patent No. 5,973,440, October
    • Nitzsche, F., Grewal, A. and Zimcik, D. (inventors). Structural Component Having Means for Actively Varying its Stiffness to Control Vibrations, U.S. Patent No. 5,973,440, October 1999.
    • (1999)
    • Nitzsche, F.1    Grewal, A.2    Zimcik, D.3
  • 5
    • 0034135721 scopus 로고    scopus 로고
    • Helicopter vibration reduction through cyclic variations in blade root stiffness
    • Anusonti-Inthra, P. and Ghandi, F., "Helicopter Vibration Reduction Through Cyclic Variations in Blade Root Stiffness," Journal of Intelligent Materials and Structures, 11(2): 153-166.
    • Journal of Intelligent Materials and Structures , vol.11 , Issue.2 , pp. 153-166
    • Anusonti-Inthra, P.1    Ghandi, F.2
  • 6
    • 3042543538 scopus 로고    scopus 로고
    • Active twist rotor blade modelling using particle-wake aerodynamics and geometrically exact beam structural dynamics
    • Cesnik, C. E. S., Opoku, D. G., Nitzsche, F. and Cheng, T., "Active twist rotor blade modelling using particle-wake aerodynamics and geometrically exact beam structural dynamics," Journal of Fluids and Structures, 19(2004): 651-668.
    • Journal of Fluids and Structures , vol.19 , Issue.2004 , pp. 651-668
    • Cesnik, C.E.S.1    Opoku, D.G.2    Nitzsche, F.3    Cheng, T.4
  • 7
    • 0020767530 scopus 로고
    • Some analysis methods for rotating systems with periodic coefficients
    • Dugundji, J. and Wendell, J. H., "Some Analysis Methods for Rotating Systems with Periodic Coefficients," AIAA Journal, Vol. 21, 1983, pp. 890-897.
    • (1983) AIAA Journal , vol.21 , pp. 890-897
    • Dugundji, J.1    Wendell, J.H.2
  • 8
    • 0035269142 scopus 로고    scopus 로고
    • Aeroelastic analysis of a helicopter blade with active impedance control at the root
    • Nitzsche, F., "Aeroelastic Analysis of a Helicopter Blade with Active Impedance Control at the Root," Canadian Aeronautics and Space Journal, Vol. 47, 2001, pp. 7-16.
    • (2001) Canadian Aeronautics and Space Journal , vol.47 , pp. 7-16
    • Nitzsche, F.1
  • 11
    • 0004192583 scopus 로고
    • Calculation of non-lifting potential flow about arbitrary three-dimensional bodies
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    • (1968) McDonnell Douglas Rep. No ES40622 , vol.ES40622
    • Hess, J.L.1    Smith, A.M.O.2
  • 12
    • 0000510678 scopus 로고
    • High order accurate vortex methods with explicit velocity kernels
    • Beale, J. T., and Majda, A., "High Order Accurate Vortex Methods With Explicit Velocity Kernels," Journal of Computational Physics, Vol. 58, pp. 188-208, 1985.
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    • Beale, J.T.1    Majda, A.2
  • 14
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  • 20
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    • The prediction of helicopter rotor discrete frequency noise
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.