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Providing Aircraft Certification Services Since 1989

T 425.438.0215



FEM ModelAeroAcoustics can conduct analysis of aircraft structures using finite element modeling or traditional stress analysis methods.  FEM analysis is tightly integrated with CAD solid modeling and loads analysis, including aerodynamic loads.  If we can't solve the problem analytically, static and/or dynamic tests of structure can be conducted using state of the art instrumentation.

  Finite Element Modeling Integrated with CAD Solid Models

  Traditional Stress Analysis Methods

  Loads Analysis Including Aerodynamic Loads

  Fatigue and Damage Tolerance Development, Assessment and Test

  Static and Dynamic Structural Tests Including Strain and Temperature Survey, Ground Vibration Tests (GVT), Flutter Test and Vibration Test (Rap Test FFT)

  Material Allowables Development

727 Strain Duke 60 Winglet

To contact us:

T 425.438.0215

F 425.438.0275