Simulation
Propeller plane - simulation Von Mises stress, internal stress, transformation and displacement
Material: Al alloy Tensile strength: 310 MPa Load Type: Force [N]
Density: 2.7 g/cm3 Young's Module: 68.9 GPa Size: 5000,000 N
Weight: 8.13372 kg Poisson constant: 0.33 ul Vector X: 5000,000 N
Area: 602853 mm2 Elastic modul: 25.9023 GPa Vector Y: 0.000 N
Volume: 3012490 mm3 Vector Z: 0.000 N
Simulation of the steering fork of a small sport aircraft
Material: Stainless steel Tensile strength: 450 MPa Load Type: Force [N]
Density: 8 g/cm3 Young's Module: 193 GPa Size: 50,000 N
Weight: 0.00082943
kg Poisson constant: 0.3 ul Vector X: 0.000 N
Area: 464.244
mm2 Elastic modul: 74.2308 GPa Vector Y: 50.000 N
Volume: 103.679
mm3 Vector Z: 0.000 N
Load disc nose gear aircraft combined force
Material: Al alloy Tensile strength: 275 MPa Load Type: Force [N]
Density: 2,7 g/cm3 Young's Module: 68,9 GPa Size: 3000,000 N
Weight: 4,71761 kg Poisson constant: 0.33 ul Vector X: 0.000 N
Area: 188767 mm2 Elastic modul: 25.9023 GPa Vector Y: 3000.000 N
Volume: 1747260 mm3 Vector Z: 0.000 N