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

Study of the NASA/LANGLEY LS(1)-0417 (GA(W)-1) Airfoil - Copy

Open Project
Copy Project
Study of the NASA/LANGLEY LS(1)-0417 (GA(W)-1) Airfoil - Copy image
views 42shares 0
KevinFireheart
KevinFireheart
Created

Last modified

Statistics
geometries 1 Geometrymeshes 4 Meshessimulations 4 Simulation setupsruns 9 Results
About this project

Measurement of the lift coefficient and drag coefficient at a certain angle of attack. - Copy

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 jprobstjprobst

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

by robertpmrobertpm

Project History

  • Bernie

    Bernie created this project

  • KevinFireheart

    KevinFireheart copied this project