Set up your own cloud-native simulation in minutes.Start Simulating Now
Homework4_Exo3
59
0Statistics
0 Geometries
0 Meshes
0 Simulation setups
0 Results
0 Geometries 0 Meshes 0 Simulation setups 0 ResultsAbout this project
A designer wants to stiffen the skin of fuselage under the transverse pressure load of 5200 lbf/in2 with the spacing of 9.25 in. The designer should choose from available stringers as shown in the following figure. The material properties of panel and stringers are given bellow.
Related Projects
Project History
cbroyard created this project