SimScale logo
Set up your own cloud-native simulation in minutes.Start Simulating Now

NACA 0012 Test Part 2

Open Project
Copy Project
NACA 0012 Test Part 2 image
0views 154shares 0
SayanS
SayanSlikes 0
Created

Last modified

Statistics
geometries 2 Geometriesmeshes 2 Meshessimulations 1 Simulation setupruns 2 Results
About this project

Incompressible simulations performed at angles of attack of 24 and 32 degrees. Simulation conditions: - 15 m/s free stream velocity - 101.325 kPa air pressire - 0.10 m chord length - 0.30 m span - approximate Reynolds number of 105 000

Share this project

Related Projects

airflow_around_a_spoiler_1 image
Tutorial - Airflow around a spoiler

by Ali_ArafatAli_Arafat

tutorial-_harmonics_analysis_of_an_airfoil_-2-2-_3 image
Tutorial: Harmonics Analysis of an Airfoil (2/2)

by simscalesimscale

tutorial-_compressible_flow_around_a_wing image
Tutorial: Compressible Flow Around a Wing

by simscalesimscale

airplane_cabin_fluid_flow_simulation image
Fluid Flow Simulation of an Airplane Cabin Ventilation

by SamPrabhuSamPrabhu

proyecto_simscale image
Drone LM RQ-170 Sentinel CFD - Drag Coefficient

by robertpmrobertpm

Project History

  • SayanS

    SayanS created this project

  • SayanS

    SayanS copied this project