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NACA 2412 modified by akssamal807 | SimScale...

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Aerospace & Defense
NACA 2412 modified

NACA 2412 modified

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Design Modification of Airfoil by Integrating Sinusoidal Leading Edge and Dimpled Surface

akssamal807

Created

Last modified

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About this project

Design Modification of Airfoil by Integrating Sinusoidal Leading Edge and Dimpled Surface

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Project History

akssamal807 created this project
over 6 years ago

Open Project

Copy Project

No visualizations or screenshots available for this project.

Project History

akssamal807 created this project
over 6 years ago

akssamal807

Created

Last modified

Statistics

0 Geometries

0 Meshes

0 Simulation setups

0 Results

About this project

Design Modification of Airfoil by Integrating Sinusoidal Leading Edge and Dimpled Surface

Related Projects

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Tutorial: Harmonics Analysis of an Airfoil (2/2)

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