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轴对称矢量喷管数值模拟及数学模型研究

On Establishing the Mathematical Model for Axisymmetric Thrust-Vectoring Nozzle

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【作者】 卢燕樊思齐马会民

【Author】 Lu Yan, Fan Siqi, Ma Huimin (Northwestern Polytechnical University, Xi′an 710072)

【机构】 西北工业大学航空动力与热力工程系西北工业大学航空动力与热力工程系 陕西西安710072陕西西安710072陕西西安710072

【摘要】 应用数值模拟方法对轴对称推力矢量喷管的内流场性能进行了研究 ,采用 Jameson提出的有限体积法计算了矢量喷管的内部流场和性能参数 ,分析了性能参数及其相关参数之间的关系 ,从而建立了轴对称推力矢量喷管的数学模型

【Abstract】 To our best knowledge, we are the first in China to establish the mathematical model needed for controlling the vector angle of axisymmetric thrust vectoring nozzle. Before establishing this model, preparatory research work must be done. Section 1 uses A. Jameson′s finite volume method to calculate the inner flow field and performance parameters of axisymmetric thrust vectoring nozzle described in Ref., and in Figs. 1 through 4 compares the calculated results with test data given in Ref.. Section 2 discusses another part of our preparatory research; it also uses Jameson’s finite volume method to calculate performance parameters for a certain type of Chinese axisymmetric thrust vectoring nozzle. Section 2 also discusses the relationships among performance parameters, geometric configuration parameters and boundary conditions. Finally, using the above mentioned relationships, section 3 establishes the mathematical model needed for controlling the vector angle of axisymmetric thrust vectoring nozzle.

  • 【文献出处】 西北工业大学学报 ,Journal of Northwestern Polytechnical University , 编辑部邮箱 ,2002年03期
  • 【分类号】V235
  • 【被引频次】14
  • 【下载频次】331
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