Set up your own cloud-native simulation in minutes.Start Simulating Now
DESIGN OF VARIABLE AREA DIFFUSER OF AIRCRAFT ENGINE
0 163 0
Statistics
0 Geometries 0 Meshes 0 Simulation setups 0 Results
About this project
COMPLEX ENGINEERING PROBLEM FOR GT: design variable area diffuser of aircraft engine with operating mach no. 0.5 to 0.1. the altitude of aircraft would be between 10000ft to 30000ft( Take dimension from commercial turbofan engine)
Related Projects
Project History
alishah created this project