Details of airfoil (aerofoil)(mh114-il) MH 114 13.02% Martin Hepperle MH 114 for a propeller for ultralight

Included below are coordinates for approximately 1,650 airfoils (Version 2.0). The UIUC Airfoil Data Site gives some background on the database. The airfoils are listed alphabetically by the airfoil filename (which is usually close to the airfoil name).

Airfoil plotter (mh114-il) MH 114 13.02% - Martin Hepperle MH 114 for a propeller for ultralight. Plot and print the shape of an airfoil (aerofoil) for your specific chord width and transformation.

2007年11月9日 · mh114.dat \ Martin Hepperle MH 114 for a propeller for ultralight \ mh114.gif\ \ \ mh115.dat \ Martin Hepperle MH 115 for a propeller for ultralight \ mh115.gif\ \ \ mh116.dat \ Martin Hepperle MH 116 for a propeller for ultralight \ mh116.gif\ \ \ mh117.dat \ Martin Hepperle MH 117 for a propeller for ultralight (tip) \ mh117.gif\ \ \

MH 114. Designed for the center region of propellers, between MH 113 and MH 115 see also MH 126, MH 112, MH 113, MH 114, MH 115, MH 116, MH 117, MH 120, MH 121. Characteristics. Thickness: 13.0%; Max. camber: 6.5%; Can be used at Reynolds numbers of 250'000 and above.

View the airfoil details page with polar diagrams for a range of Reynolds numbers. View and plot a full size plan of the airfoil to your chord width. The camber, thickness can be adjusted and the …

Bulk download of polars in Excel format: mh114.xlsx. Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.

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从MH117翼型到MH114翼型，弯度逐渐增大，零升迎角的绝对值也在逐渐增大（即图像与横轴的交点越靠左），并且在同一迎角下所对应的最大升力系数也越大。 其中 NACA0015 的图像经过了原点，是因为对称翼型在迎角为零时，没有升力。 压力中心（压心） 翼面的分布压力有个合力（即升力），这个合力和翼弦的交点称为压力中心，又叫压心。 所有的分布压力相对于这一点的和力矩（假设抬头力矩为正，低头力矩为负）为零。