A Simple Method for Calculating LAE of Helicopter Noise.

Bibliographic Information

Other Title
  • ヘリコプター騒音のLAEの簡易予測方法

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Description

We considered a method for calculating the sound exposure level (LAE) of helicopter noise. It was assumed that helicopters have no directivity and that the propagation of sound can be expressed in a simple function of distance from an observation point to a sound source. We derived a formula for LAE by integrating the sound energy along a finite or an infinite flight segment. And we classified the value of power level into three groups by the maximum takeoff weight. The values calculated from the formula agree with the results of test flights in which three types of helicopters each took three moving operations of approach, takeoff and level flyover.

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Details 詳細情報について

  • CRID
    1390001204767295488
  • NII Article ID
    130003656908
  • DOI
    10.11372/souonseigyo1977.20.385
  • ISSN
    18837506
    03868761
  • Text Lang
    ja
  • Data Source
    • JaLC
    • CiNii Articles
  • Abstract License Flag
    Disallowed

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