| 燃气轮机弹性数学模型 |
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| 引用本文： | 朱行健,W.F.O''Brien.燃气轮机弹性数学模型[J].航空动力学报,1987,2(4):312-316,369. |
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| 作者姓名： | 朱行健 W.F.O'Brien |
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| 作者单位： | 1.北京航空学院 |
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| 摘 要： | 本文根据燃气轮机各部件的基本工作原理,从已有部件的试验特性推导出具有不同设计参数的新设计部件的特性。将这种方法与燃气轮机数学模型相结合,构成设计参数可以变化的燃气轮机“弹性”数学模型。
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| 收稿时间： | 4/1/1987 12:00:00 AM |
ELASTICITY MODEL FOR SCALING GAS TURBINE PERFORMANCE PREDICTION |
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| Zhu Xingjian and W. F. O''Brien.ELASTICITY MODEL FOR SCALING GAS TURBINE PERFORMANCE PREDICTION[J].Journal of Aerospace Power,1987,2(4):312-316,369. |
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| Authors: | Zhu Xingjian and W F O'Brien |
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| Institution: | 1.Beijing Institute of Aeronautics and Astronautics2.Virginia Polytechnic Institute and State University |
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| Abstract: | Before a gas turbine is designed, many candidate designs with different values of designparameters must be studied. Calculation of design and off-design performances of proposedengines is needed, but actual component maps do not exist. In this paper, new scaling laws are developed and shown to produce component maps and estimates of new engine performanceswhich are predicted to be close to the actual values. This "elasticity"model is based on the fundamental operating principles of the components. |
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