Aeroacoustic data for four NACA series aerofoils

This dataset provides near-field hydrodynamic and far-field acoustic data that has been acquired in the aeroacoustic wind tunnel facility at the University of Bristol. The data has been collected as part of a PhD research project into the noise generated by an aerofoil undergoing stall. The purpose of making the dataset publicly accessible is to facilitate the validation and development of predictive aeroacoustic models, to provide validation data for aeroacoustic simulations, and to provide comparative data for other experimental aeroacoustic test campaigns.

搜集汇总

背景与挑战

背景概述

该数据集提供了四个NACA系列翼型（NACA 0012、0024、16-506、16-616）的气动声学实验数据，包含近场流体动力学和远场声学测量结果，由布里斯托大学风洞设施采集。数据旨在支持气动声学预测模型的验证与开发、为模拟提供基准，并促进实验比较，重点关注翼型失速噪声现象，总大小为374.5 MiB，发布于2024年。