SDAERO |
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Transonic flow calculations in minutes rather than hours - SDAERO couples small disturbance potential flow and integral boundary layer methods to facilitate the rapid design and analysis of wings and bodies in the transonic regime.
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Generic Transport Optimized for Lift/Drag using Aeropointer.
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Small Business Jet Wing Design Performed with SDAERO
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Simple input requirements and clearly tabulated output are combined with OMNI3D plotting capability.
SDAERO provides rapid estimation of lift, drag and separation onset throughout the aircraft high-speed flight envelope.
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Wing-body optimization for performance and loads is available using the AeroPointerTM software package.
Non-linear aerodynamic loads calculation for multiple flight conditions are made in a fraction of the time required by Euler or Navier-Stokes codes.
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KC-135 Winglet Modification Analysis
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727 Wing Pressure Distributions
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System Requirements |
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This software is available for the following systems: linux
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Additional Information |
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