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Analysis and Control of Flow and Flutter in Aeroengines

Analysis and Control of Flow and Flutter in Aeroengines
航空发动机流动与颤振分析与控制
批准号:
0072191
负责人:
Bjorn Birnir
金额:
$10.98万
依托单位国家:
美国
项目类别:
Continuing Grant
财政年份:
2000
资助国家:
美国
项目状态:
已结题
起止时间:
2000-08-01 至 2003-07-31

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中文摘要
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英文摘要
0072191BirnirIn a program of analytical and computational investigations, the investigator will develop control theory to make jet engines lighter, more efficient and safer. Surge and stall are instabilities in the flow of air through the engines; flutter is an oscillation of the blades compressing the air. These instabilities decrease the efficiency of the engine and can be dangerous. The control theory aims at controlling all of these instabilities.If lighter, more fuel efficient and safer aircraft engines are to be made the current technology needs to be improved. This research tries to accomplishes this goal by first developing a mathematical model for the jet engine, then simulating this model of the engine on a computer and using the results to figure out how to design a much more efficient and safer jet engine. Then this design is implemented and checked in the laboratory. Similar technology is also used to compress rocket fuel before combustion and an optimization of the technology as a whole may lead to cheaper space travel.
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Scientific Computing Research Environments for the Mathematical Sciences (SCREMS)
Applications of Qualitative Analysis of Nonlinear PDE's
Mathematical Sciences: Attractors, Weak-Turbulence and Nonexistence of Breathers
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