AeroAcoustics 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