低速增压风洞气流参数的测量方法

本文根据低速增压风洞的工作性能包线，详细分析了马赫数Ma和速压Q的测量误差，同时给出了可行的测量方案及其科学的计算方法。     

低速风洞大迎角实验的不确定度评估技术与工程应用

本文将AGARD-AR-304不确定度评估方法推广到大迎角领域，给出计算低速风洞大（小）迎角实验不确定度的工程方法。相应的计算软件已成功地用于国内主力低速风洞实验的不确定度评估，且首次给出了我国主力低速风洞大（小）迎角实验的不确定度水平。     

空气压缩机的经济运行及使用寿命初探

以空压机技术理论为依据，结合实践经验，分析了空压机常见故障及解决方法。阐述了延长空压机使用寿命的途径，提出了空压机处于最佳运行状态的措施。     

矢量控制技术在风洞动力系统中的应用

介绍了无速度传感器矢量控制技术的基本原理,通过对HY 750开口回流低速风洞的实验数据分析,从具体精度指标上对风洞动力系统应用矢量控制的效果进行了评估。结果表明:矢量控制技术在HY 750风洞动力系统中的应用是成功的,能够有效提高动压稳定性,改善流场品质。     

DEVELOPMENT FOR HIGH PRECISION SIX COMPONENT STRAIN GAUGE BALANCE

The measurement accuracy of a wind tunnel balance is the key factor to improve the measurement accuracy for a test model in the wind tunnel. In order to improve the measurement accuracy of the wind tunnel balance, a great deal of investigation is carried out in China. This paper summarizes a program to improve the measurement accuracy of wind tunnel balances. In the program, the investigation is carried out in three aspects (1) designing a drag component of the balance in low interactions (2) choosing high quality foil strain gauges with temperature self-compensation (3) choosing the excellent gauges and mounting them meticulously. As an example, these research achievements are applied in a φ18 six component balance. The measurement accuracy of a GB-04 standard model in a transonic wind tunnel with the φ18 six component balance comes up to the advanced world standard.