发动机用扩压器性能及扩压器后射流数值分析

(西安航天动力试验技术研究所,陕西 西安 710100)

扩压器性能; 燃气射流; 数值研究; 环境设计

Numerical analysis of the performance of the diffuser for rocket engine and the gas jet after the diffuser
HE Hong,DING Jiawei,LENG Haifeng,YU Fanchao,ZHANG Yuhao

(Xi'an Aerospace Propulsion Test Technology Institute,Xi'an 710100,China)

performance of diffuser; gas jet; numerical study; environmental design

备注

扩压器是火箭发动机进行高空模拟试验的重要地面设备,针对某空气泄入式圆筒型扩压器设计参数进行了数值研究,同时对该扩压器后的燃气射流进行了分析。计算结果表明,扩压器直径是影响扩压器性能的一个重要参数,在满足喷管出口满流的前提下,当扩压器直径增大时,带来的是总压损失逐渐增大,扩压器内激波串的强度逐渐增强; 长径比并不是一个影响扩压器流场和起动情况的独立参数,该参数的选取与发动机工况状态和结构状态相关; 泄入间隙的选择可根据发动机的工况进行设计。对扩压器后的燃气射流计算表明,与不带扩压器的喷管燃气射流相比,由于燃气在扩压器内总压损失较自由射流小,扩压器后的燃气射流具有影响区域范围大的特点,该计算结果可为发动机地面试验不同条件下燃气射流提供一定的预示,对试验过程中燃气射流引起的环境设计提供借鉴。

The diffuser is an important ground equipment for high altitude simulation test of rocket engines. The design parameters of an air-bleed cylinder diffuser were studied numerically,and the gas jet after the diffuser was analyzed. The results show that the diffuser diameter is an important parameter affecting the diffuser performance. When the diffuser diameter increases,the total pressure loss increases and the intensity of shock wave in the diffuser increases. The length-diameter ratio is not an independent parameter affecting the diffuser flow field and start-up. The selection of the parameters is related to the engine working condition and structure condition,and the selection of the leakage gap can be designed according to the engine working condition. The calculation of the gas jet after the diffuser shows that,compared with the nozzle gas jet without the diffuser,the gas jet after the diffuser has the characteristics of large area because the total pressure loss of the gas in the diffuser is smaller than that of the free jet. It provides a reference for the environmental design caused by gas jet during the test.

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