摘要
Pressure sensitive paint (PSP) is an optical technique used in wind-tunnel models. It is becoming an alternative to the classical method of pressure taps. This study applies a polymer-ceramic PSP in compressible cylindrical cavity and convex-corner flows. Using prior calibration and a wind-off image, the full-field pressure pattern is obtained. The effect of temperature on the model's surface is measured using temperature sensitive paint (TSP), and the accuracy of the measurements is addressed. For a compressible convex-corner flow, in-situ calibration is required when there are significant pressure gradients.
原文 | English |
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頁(從 - 到) | 265-274 |
頁數 | 10 |
期刊 | Journal of Aeronautics, Astronautics and Aviation |
卷 | 51 |
發行號 | 3 |
DOIs | |
出版狀態 | Published - 2019 9月 1 |
All Science Journal Classification (ASJC) codes
- 航空工程
- 空間與行星科學