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模拟来流参数误差对固体冲压发动机地面试验结果影响的评估
引用本文:李进贤,张林,韩迎龙,曹琪.模拟来流参数误差对固体冲压发动机地面试验结果影响的评估[J].固体火箭技术,2011,34(1):57-60.
作者姓名:李进贤  张林  韩迎龙  曹琪
作者单位:西北工业大学航天学院,西安,710072
基金项目:装备预先研究项目(No.51328020106)
摘    要:在固冲发动机地面试验中,模拟来流误差对试验结果有很大影响,开展相关影响评估研究具有重要的理论意义和工程价值.基于一维气动理论,结合某试验固冲发动机,采用小偏差方法评估模拟来流误差对试验结果的影响,给出了发动机性能参数时模拟误差的敏感系数和小偏差方法的适用范围,提出了一套较完整的考虑模拟误差的固冲发动机性能计算方法和固冲...

关 键 词:固体冲压发动机  试验技术  小偏差方法  敏感系数

Evaluating of influence of simulating coming flow error on the SDR ground test
LI Jin-xian,ZHANG Lin,HAN Ying-long,CAO Qi.Evaluating of influence of simulating coming flow error on the SDR ground test[J].Journal of Solid Rocket Technology,2011,34(1):57-60.
Authors:LI Jin-xian  ZHANG Lin  HAN Ying-long  CAO Qi
Institution:LI Jin-xian,ZHANG Lin,HAN Ying-long,CAO Qi (College of Astronautics,Northwestern Polytechnical University,Xi'an 710072,China)
Abstract:In the ground test of solid ducted rocket(SDR),influence of the simulated coming flow error on the test result is very significant,so the research of related influence evaluation has an important theory meaning and engineering value.Based on one-dimension aerodynamics theory and combined with some type of test solid ducted rocket,the influence of simulated coming flow error to ground test of the SDR was evaluated by means of the small deviation model to provide the sensitivity coefficients of motor performa...
Keywords:solid ducted rocket  test technology  small deviation model  sensitivity coefficients  
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