Your trusted partner on the road to PLM THE MAIN EVENTS SOFTWARE ABOUT COMPANY VIDEO CONTACTS Our certifications Dassault SystemesMSC SoftwareIMS SoftwareSimufactE3 Series Copyright © TECHPROM CJSC 2007-2016 All rights reserved.

Your trusted partner on the road to PLM THE MAIN EVENTS SOFTWARE ABOUT COMPANY VIDEO CONTACTS Simufact.joining - Simulates mechanical joining. Simufact.joining has been specially designed for mechanical joining. Rivets, or bolts - all processes can be modeled in Simufact.joining. The focus is on the joining process itself: riveting, material flows with joining parts, sheet deformation, residual forces, etc. Moreover, the size of the association and its behavior under the external load (for example, static and dynamic loads). Dassault SystemesMSC SoftwareIMS SoftwareSimufactE3 Series Copyright © TECHPROM CJSC 2007-2016 All rights reserved.

Your trusted partner on the road to PLM THE MAIN EVENTS SOFTWARE ABOUT COMPANY VIDEO CONTACTS FlightLoads is a comprehensive analysis of aeroelastic, dynamic and strength characteristics of aircraft. FlighLoads is an application designed to prepare computational models for solving subsonic, supersonic, stationary and non-stationary aeroelasticity problems. Using FlighLoads, the following types of tasks are solved: balancing elastic or "rigid" aircraft; flutter problem; calculating the response of an elastic aircraft to an external impact (gust or impact); design optimization. The aeroelastic computational model consists of elastic-mass and aerodynamic models. The elastic-mass model is created using standard Patran preprocessor tools , and the aerodynamic model is created in the environmentPatran using the capabilities of the FlighLoads module . The MSC Nastran or MD Nastran software packages are used as a solver for the above aeroelasticity problems . The following aerodynamic methods are available for calculating aerodynamic loads: · Doublet-Lattice Method (DLM); Subsonic Wing-Body Interference Theory (Slender Bodies); ZONA51; · Mach Box Method; Strip Theory Piston Theory. Using the FlightLoads module also provides additional (special) capabilities for analyzing the results of solving an aeroelastic problem in the Patran postprocessor environment . Dassault SystemesMSC SoftwareIMS SoftwareSimufactE3 Series Copyright © ЗАО ТЕХПРОМ 2007-2016 Все права защищены.