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超燃冲压发动机性能参数测量不确定度分析

  • Beijing Institute of Technology
  • Science and Technology on Scramjet Laboratory
  • China Aerospace Science and Industry Corporation

科研成果: 期刊稿件 › 文章 › 同行评审

摘要

Based on wind tunnel test uncertainty assessment of AIAA S-071A-1999 and the uncertainty study for the wind tunnel testing,aeroengine performance testing and rocket ground testing in the international space power community,an uncertainty analysis method for the scramjet performance testing was established,and corresponding analysis was given.Results showed that the uncertainty induced by the free-jet testing measurement was predominant in evaluating the overall scramjet performance,and the bias limit was over 90% in the uncertainty of scramjet performance parameters measurements.In conclusion,some valuable results and suggestions about the uncertainty of overall performance of scramjet were obtained,and these results can improve the accuracy in scramjet performance parameters measurements,showing prominent application prospect in scramjet development.

投稿的翻译标题Uncertainty analysis in scramjet performance parameters measurements
源语言繁体中文
页(从-至)2421-2428
页数8
期刊Hangkong Dongli Xuebao/Journal of Aerospace Power
卷35
期11
DOI
出版状态已出版 - 11月 2020

关键词

  • Bias limit
  • Free-jet test
  • Overall performance
  • Precision limit
  • Scramjet
  • Uncertainty

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