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Preliminary Design

 

During the preliminary design phase each part of the aircraft has been analyzed. Aerodynamic efficiency, stability and control, structures, propulsion and inlets have all been studied in detail. Even though the overall configuration was defined in the conceptual design phase, some changes in the geometry occurred. The resulting configuration is an inherently stable aircraft with a total endurance greater than 10 hours.

 

  • The HCUAV external geometry during the preliminary design phase
  • Preliminary structural layout of the HCUAV
  • Preliminary CFD computations
  • Flow development on around the HCUAV
The HCUAV external geometry during the preliminary design phase

The HCUAV external geometry during the preliminary design phase

Preliminary structural layout of the HCUAV

Preliminary structural layout of the HCUAV

Preliminary CFD computations

Preliminary CFD computations

Flow development on around the HCUAV

Flow development on around the HCUAV

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