Data Set Information:

NASA数据集包括不同风洞速度和攻角下不同尺寸的NACA 0012翼型。翼型的跨度和观察者的位置在所有实验中都是相同的。

Attribute Information:

此问题有以下输入：
1.频率，以赫兹为单位。
2.攻角，以度为单位。
3.弦长，以米为单位。
4.自由流速度，以米/秒为单位。
5.吸入侧位移厚度，单位为米。
唯一的输出是：
6.标度声压级，单位为分贝。

Relevant Papers:

T.F. Brooks, D.S. Pope, and A.M. Marcolini.
Airfoil self-noise and prediction.
Technical report, NASA RP-1218, July 1989.

K. Lau.
A neural networks approach for aerofoil noise prediction.
Mastera€?s thesis, Department of Aeronautics.
Imperial College of Science, Technology and Medicine (London, United Kingdom), 2006.

R. Lopez.
Neural Networks for Variational Problems in Engineering.
PhD Thesis, Technical University of Catalonia, 2008.

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