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Details of Side Load Test Data and Analysis for a Truncated Ideal Contour Nozzle and a Parabolic Contour Nozzle

机译:截断的理想轮廓喷嘴和抛物线轮廓喷嘴的侧向载荷测试数据和分析的详细信息

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摘要

Two cold flow subscale nozzles were tested for side load characteristics during simulated nozzle start transients. The two test article contours were a truncated ideal and a parabolic. The current paper is an extension of a 2009 AIAA JPC paper on the test results for the same two nozzle test articles. The side load moments were measured with the strain tube approach in MSFC s Nozzle Test Facility. The processing techniques implemented to convert the strain gage signals into side load moment data are explained. Nozzle wall pressure profiles for separated nozzle flow at many NPRs are presented and discussed in detail. The effect of the test cell diffuser inlet on the parabolic nozzle s wall pressure profiles for separated flow is shown. The maximum measured side load moments for the two contours are compared. The truncated ideal contour s peak side load moment was 45% of that of the parabolic contour. The calculated side load moments, via mean-plus-three-standard-deviations at each nozzle pressure ratio, reproduced the characteristics and absolute values of measured maximums for both contours. The effect of facility vibration on the measured side load moments is quantified and the effect on uncertainty is calculated. The nozzle contour designs are discussed and the impact of a minor fabrication flaw in the nozzle contours is explained.
机译:在模拟的喷嘴启动瞬态过程中,测试了两个冷流量副刻度喷嘴的侧向载荷特性。两个测试物品的轮廓是截断的理想曲线和抛物线。本文是对相同的两个喷嘴测试文章的测试结果的2009 AIAA JPC论文的扩展。在MSFC的喷嘴测试设备中使用应变管方法测量了侧向载荷力矩。解释了将应变计信号转换成侧向力矩数据的处理技术。给出并详细讨论了在许多NPR时分开的喷嘴流的喷嘴壁压力曲线。示出了测试单元扩散器入口对抛物线形喷嘴的壁流压力分布的影响。比较两个轮廓的最大测得的侧向负载力矩。截断的理想轮廓的峰值侧载荷力矩为抛物线轮廓的峰值载荷的45%。通过每个喷嘴压力比处的平均值加三个标准偏差计算出的侧向负载力矩,再现了两个轮廓的最大测量值的特性和绝对值。量化了设备振动对测得的侧向载荷力矩的影响,并计算了对不确定性的影响。讨论了喷嘴轮廓设计,并解释了喷嘴轮廓中轻微制造缺陷的影响。

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