二元推力矢量喷管气动-热-结构耦合特性研究

Study on Aerodynamic-Thermal-Structural Coupling Characteristics of Two-Dimensional Thrust Vectoring Nozzle

  • 摘要: 矢量喷管结构作为矢量发动机区别于其他类型发动机的显著特征,具有结构复杂、载荷环境恶劣等缺点。喷管处于发动机高温区,高温会使喷管的材料、结构力学性能退化,会降低结构的安全性、可靠性。要实现对二元矢量喷管结构可靠性和完整性评估,必须测量分析喷管热载荷和结构载荷参数,故需要对该喷管的特性进行分析研究。该文建立了不同偏转角度下的二元矢量喷管计算模型,采用基于流固热耦合的数值计算方法对二元矢量喷管的结构特性进行了分析研究,并获取了不同工况下的喷管载荷特性。所研究内容可以为二元矢量喷管的结构特性及可靠性和完整性评估提供一定的参考和借鉴。

     

    Abstract: Vector nozzle structure, as a significant feature of vector engine distinguishing from other types of engines, has the disadvantages of complex structure and harsh loading environment.The nozzle is in the high temperature region of the engine, and the high temperature will degrade the material and structural mechanical properties of the nozzle, which will reduce the safety and reliability of the structure.To realize the assessment of the reliability and integrity of the binary vector nozzle structure, it must measure and analyze the nozzle thermal load and structural load parameters, so it is necessary to analyze and study the characteristics of this nozzle.The paper established the binary vector nozzle calculation model under different deflection angles, analyzed and researched the structural characteristics of the binary vector nozzle by using the numerical calculation method based on fluid-solid-thermal coupling, and obtained the nozzle load characteristics under different working conditions.The findings of this study can provide certain reference and insight for the structural characteristics, reliability and integrity assessment of the binary vector nozzle.

     

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