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Wind Tunnel Airfoil Measurement by Leybold

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Management number 211309265 Release Date 2026/04/04 List Price $36.00 Model Number 211309265
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In experiment P1.8.7.1, the air resistance and lift of an airfoil are measured based on its angle of attack. These measurements are plotted in a polar diagram, allowing for the determination of the optimal angle of attack. Students also measure airfoils they've designed themselves, aiming to find the shape that minimizes the quotient of air resistance to lift at a given angle of attack.

  • Experiment P1.8.7.1: Measure air resistance and lift of an airfoil based on angle of attack
  • Graphical representation: Plot air resistance against lift with angle of attack as parameter
  • Determine optimal angle of attack from the polar diagram
  • Students conduct similar measurements on custom-designed airfoils
  • Objective: Identify airfoil shape for minimal air resistance to lift ratio at a given angle
Brand Name leybold
Model Number P1.8.7.1

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