Airfoil for Volos Wing analysis

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Post-Processor Screenshot - PostProcessorScreenshot
Post-Processor Screenshot - PostProcessorScreenshot
PostProcessorScreenshot
2D
Post-Processor Screenshot - PostProcessorScreenshot
PostProcessorScreenshot
2D
EPPLER_1210__20_deg - Geometry
Geometry
3D
EPPLER_1210__0_deg - Geometry
Geometry
3D
NACA_63-615 - Geometry
Geometry
3D
NACA_65-410 - Geometry
Geometry
3D
EPPLER_1210__10_deg - Geometry
Geometry
3D
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Volos1
Volos1
Created

over 7 years ago

Last modified

over 7 years ago

Statistics
geometries 5 Geometries
meshes 5 Meshes
simulations 11 Simulation setups
runs 75 Results
About this project

Testing NACA 63-615 vs NACA 65-410 vs EPPLER 1210. Chord length is 0.3 m Testing EPPLER 1210 with 0, 10, 20 deg of chord flex

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Project History

  • Volos1

    Volos1 created this project

    over 7 years ago

Airfoil for Volos Wing analysis by Volos1 | SimScale