Princeton Dynamic Stall Database: Upward ramp-type pitching motions
收藏DataCite Commons2024-10-21 更新2024-07-13 收录
下载链接：
https://datacommons.princeton.edu/discovery/doi/10.34770/b3vq-sw14
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资源简介：
This data set contains data of a NACA 0021 airfoil as it undergoes upward
ramp-type pitching motions at high Reynolds numbers and low Mach numbers.
The parametric study covers a wide range of chord Reynolds numbers,
reduced frequencies and pitching geometries characterized by varying mean
angle and angle amplitude. The data were acquired in the High Reynolds
number Test Facility at Princeton University, which is a closed-loop wind
tunnel that can be pressurized up to 23 MPa and allowed for variation of
the chord Reynolds number over a range of 5.0 × 10^5 ≤ Re_c ≤ 5.5 × 10^6.
Data were acquired using 32 pressure taps along the surface of the
airfoil. The data are the phase-averaged results of 150 individual
half-cycles for any given test case.
提供机构：
Princeton University
创建时间：
2021-03-31
