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IPC-80亚、跨、超音速风洞弹丸及飞行器试验测试系统
引用本文:王崇和,谭俊杰,吴军基,张慧丽. IPC-80亚、跨、超音速风洞弹丸及飞行器试验测试系统[J]. 测试技术学报, 1996, 0(2)
作者姓名:王崇和  谭俊杰  吴军基  张慧丽
作者单位:南京理工大学,南京理工大学,南京理工大学,南京理工大学 南京 210094,南京 210094,南京 210094,南京 210094
摘    要:本文主要介绍亚、跨、超音速风洞基本结构及气动原理,新配置的IPC-80测试系统。论述了弹丸及飞行器气动试验模拟信号处理、变换采样、数字量取真、模型迎角和阀位循环码读取方法,对标模动校作了测试精度考核。

关 键 词:弹丸气动测试  风洞测试系统  信号处理  变换与采样  标模动校

TRIAL TESTING SYSTEM FOR PROJECTILE AND VEHICLE OF 1PC-80 SUBSONIC, TRANSONIC AND SUPERSONIC WIND TUNNEL
Wang Chonghe Tan Junjie Wu Junji Zhang Huili. TRIAL TESTING SYSTEM FOR PROJECTILE AND VEHICLE OF 1PC-80 SUBSONIC, TRANSONIC AND SUPERSONIC WIND TUNNEL[J]. Journal of Test and Measurement Techol, 1996, 0(2)
Authors:Wang Chonghe Tan Junjie Wu Junji Zhang Huili
Abstract:This article mainly introduces the fundamental structure and aerodynamical principle of subsonic, transonic and supersonic wind tunnel and a new allocate testing system of IPC-80 for projectile and vehicle. Also it details analog signal processing, transformation and sampling, data picking of aerodynamical test of projectile and vehicle. reading method of circulation code of model angle and valve place. Tacking accuracy check for dynamical calibrate of standard model.
Keywords:projectile aerodynamical test  wind tunnel testing system  signal processing  transformation and sampling  dynamic calibrate of standard model
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