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STRUCTURAL RESPONSE UNDER TURBULENT FLOW EXCITATIONS

机译:湍流激励下的结构响应

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摘要

In this report three problems of random vibration are discussed. In each case the external excitation is a turbulent flow. The first two problems, an airplane flying into atmospheric turbulence and a panel-like structure exposed to boundary-layer pressure fluctuation, are treated as linear problems. It is shown that if Taylor's hypothesis ofna frozen turbulence field is valid then the calculation can be greatly simplified using a spectral analysis in the wave-number domain. However, if decay in the turbulence is appreciable a superposition scheme can still be used to retain as much computational advantage of the wave-number domain analysis as possible.

著录项

  • 作者

    Y. K. Lin;

  • 作者单位
  • 年度 1976
  • 页码 1-52
  • 总页数 52
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 工业技术;
  • 关键词

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