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A Finite Element Method to Predict Internal Noise Levels at Discrete Frequencies for a Partially Composite Helicopter Fuselage

A Finite Element Method to Predict Internal Noise Levels at Discrete Frequencies for a Partially Composite Helicopter Fuselage

  • Presented at Forum 45
  • 12 pages
  • SKU # : 45_0_010

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A Finite Element Method to Predict Internal Noise Levels at Discrete Frequencies for a Partially Composite Helicopter Fuselage

Authors / Details: F. Chabas, J.M. David, A. Desanti, N. Meidinger, and C. Soize, ONERA, and M. Dussac, P. Martin and H.J. Marze, Aerospatiale