| 1. | Linear interpolation method for processing the test data of five - hole probes
五孔探针实验数据处理的线性插值法 |
| 2. | Finally , the seven - hole probe experiment was made on the wake flow of the fuselage with empennage and engine cabins
并应用微型总压管进行了后体的边界层测量实验，得到了边界层平均速度分布。 |
| 3. | Predictions with the reynolds stress model ( rsm ) were in reasonable agreement with experimental results measured by intelligent five - hole probe
计算结果与用五孔探针测试的气相流场实验结果吻合很好。 |
| 4. | Finally measurement of the flow field in the rotating disk with a five - hole probe is demonstrated feasible by the numerical simulation
最后，通过数值模拟预测了在该旋转盘试验中是可以用五孔探针对流场进行测量的。 |
| 5. | The seven - hole probe ( shp ) is a device which can simultaneously measure the pressure and velocities of the steady flow , especially at large angles
作为一种可以同时获得流动速度的大小、方向、以及总压和静压的气动测量装置,七孔探针能够被广泛应用于各种大角度的流动测量。 |
| 6. | But now there hasn ’ t any measure system for seven - hole probe which can integrate pressure data acquisition and data processing together . so it costs much time to complete the shp calibration and the probe use
但是目前七孔探针作为流场测试装置并没有相应的测试系统与之配套,数据的采集与处理并没有一体化,所以七孔探针校准和使用繁琐耗时。 |
| 7. | Firstly , the numerical simulation was performed on the fuselage by solving the incompressible n - s equation . secondly , with the aid of flow visualization and seven - hole probe experiment on the fuselage , the afterbody wake flow was investigated clearly
机身后体属于机身的一部分，本文首先进行了单独机身的数值计算，得到了机身表面的压力分布；其次，本文对单独机身模型进行了实验研究。 |
