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Snowcone Airfoil Shear Stress Model

Aaron Holben
Organization: Northrop Grumman
Department: ATDC
Revision date


This notebook is a demonstration to help show how mathematica is useful in Aerospace Structural analysis. This specific example models a "snow cone" airfoil that has a shear stress model that is developed from the ground up. The end has an interactive model that allows you to adjust the position of forces V2 and V3 (Lift and Drag) to see how much change of shear stress occurs in each segment of the whole airfoil.

*Engineering > Aeronautical and Astronautical Engineering

Aerospace, Structures, Demonstration, Shear Stress, Analysis, Aerospace Structures, Thin wall, Airfoil, Shear Flow, Twist Rate
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InteractiveSnowcone.nb (198.1 KB) - Mathematica Notebook