Set up your own cloud-native simulation in minutes.Start Simulating Now
NACA 64015A Swept Back Wing
2317
23Statistics
2 Geometries
1 Mesh
1 Simulation setup
1 Result
2 Geometries 1 Mesh 1 Simulation setup 1 ResultAbout this project
CFD analysis to verify the experimental results carried out on NACA 64015A Swpetback wing at AoA zero degree and Sweep angle 20 degrees. Reference: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19980227185.pdf
Related Projects
by Ali_ArafatAli_Arafat
Project History
Adithya3090 created this project