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Analyses des contraintes

Our highly qualified specialists come mostly from aerospace industry and have a lot of experience which they gained through the work on aircraft projects L410, L420, L610 and ZLIN.

Static Stress Analyses

  • Stress analyses by methods of standard strength and elasticity theory
  • Analyses of bar structures and mechanisms
  • Creation of models of parts and assemblies for analyses by method of finite elements (preprocessing in systems ANSA, FEMAP, PATRAN, ANSYS, HyperWorks/HyperMesh)
  • Linear and non-linear analyses by method of finite elements using systems MSC/NASTRAN, ANSYS, MARC
  • Solution of optimalization tasks in HyperWorks/Optistruct system
  • Evaluation of fatigue strength and service life
  • Mass analyses and optimization

Dynamic Analyses

  • Modal analyses of design including their optimization
  • Sensitivity analyses for elimination of noise and vibration
  • Non-linear dynamic simulations of real structures (geometrical and material non-linearity, contact tasks,combination with thermal tasks) - MARC
  • Simulations of systems of many bodies with their kinematics and dynamic dependence - ADAMS
  • Modeling dynamic and mechatronic system and special dynamic problems in the system MATLAB, linear simulation of dynamic actions for excitation in time and spectral area
  • Analysis of structural vibrations spreading
  • Simulations of crash tests

Aerodynamics

  • Aerodynamic analyses (geometry and systems of the airplane from the viewpoint of performances, stability and controllability, creation of groundwork documents for stress analyses)
  • Setting the flight development and certification tests, methodology and evaluation
  • Certification analyses (flight characteristics, performances, consequences of failures for reliability analyses)
  • Preparation of data and procedures for the flight manual
  • Route and economic analyses
  • Support for customers at solving nonstandard operation conditions
Model of the tail part of Ae270 airplane - systems FEMAP&MSC/NASTRANStress and deformation analysis of the front part of airplane fuselage - ANSYS systemtress and deformation analysis of VUT100 airplane - systems FEMAP&MSC/NASTRAN
Distribution of pressure on the wing profile with the icing imitator
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