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 。
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.
出处
《西北工业大学学报》
EI
CAS
CSCD
北大核心
2002年第3期383-386,共4页
Journal of Northwestern Polytechnical University
关键词
轴对称
矢量喷管
数值模拟
有限体积法
数学模型
推力矢量
飞机
axisymmetric thrust vectoring nozzle, finite volume method, mathematical model, vector angle, control
