External Aerodynamics - Aerospace

ICON has demonstrated the capacity to reproduce experimental results for a wide range of Mach number including transonic and supersonic cases.

Verification and validation of external aerodynamics results were carried out on classic cases such as the Onera M6 wing, the DLR F6 wing/body/nacelle/pylon or the NASA X778 hammerhead launcher. ICON benefits from this trust in its tools to deliver high standard external aerodynamics studies for the aerospace industry.

Example of key features covered in external aerodynamics are:

  • Aerodynamics force coefficients and center of balance

  • Contour of Mach number, pressure coefficient, yPlus, wall shear stress, Q-criterion etc.

  • Frequency response analysis

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