首页> 外文会议>18th AIAA Aerospace Ground Testing Conference June 20-23, 1994/Colorado Springs, CO >Fast-Response, Electronically-Scanned Multi-Port Pressure System for Low-Pressure Hypersonic Wind Tunnel Applications
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Fast-Response, Electronically-Scanned Multi-Port Pressure System for Low-Pressure Hypersonic Wind Tunnel Applications

机译:用于低压高超音速风洞应用的快速响应电子扫描多端口压力系统

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摘要

A fast-response, multi-port, electronically-scanned pressure (ESP) system applicable to very low pressure hypersonic wind tunnel environments has been developed and demonstrated. The system incorporates a Pressure Systems Incorporated (PSI) Model 8400 pressure measurement system with remote processor. and two 48-port PSI ESP modules of 0.36 psid and 1.0 psid full-scale-output, respectively. To achieve minimum pressure lag time, the modules are mounted internal to a variable-geometry, 10.39 in. long, 4,00 in. base diameter wind tunnel model, and are provided with a zero reference to yield absolute presure. The use of minimum length tubing has led to observed pressure lag times of 0.3 sec or less for all pressure ports and flow conditions. Absolute pressure measurement accuracy is typically+/-0.001 psia. The fast response and high accuracy make feasible the design and execution of precision CFD code validation experiments in low-pressure hypersonic wind tunnel flows.
机译:已经开发并展示了适用于超低压超音速风洞环境的快速响应,多端口电子扫描压力(ESP)系统。该系统集成了带有远程处理器的压力系统集成(PSI)8400型压力测量系统。两个分别为0.36 psid和1.0 psid满量程输出的48端口PSI ESP模块。为了获得最小的压力滞后时间,将模块安装在10.39英寸长,4.0英寸基本直径风洞模型的可变几何形状内部,并提供零基准以产生绝对压力。在所有压力端口和流量条件下,使用最小长度的管道导致观察到的压力滞后时间为0.3秒或更短。绝对压力测量精度通常为+/- 0.001 psia。快速响应和高精度使低压高超音速风洞流中精密CFD代码验证实验的设计和执行成为可能。

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