Mohammed

Last seen: 1 year 前 | 自 2022 起处于活动状态

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统计学

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How to derive 3D Lift and Drag Coefficients of a Rectangular Wing Sail from 2D Airfoil Profile Section
Iam currently working on modeling of wing sail for ship, which is same a a rectangular wing with a unifrom airfoil cross sectio...

1 year 前 | 1 个回答 | 0

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How can I make polar plots with coordinates -180 to 180 instead of 0 to 360
I need to make a plot for lift generated by an air foil for different angle of attacks from -180 degree to 180 degree. I have th...

2 years 前 | 1 个回答 | 0

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