To the SUAVE community,

Our Christmas Gift to you is SUAVE 2.3! This lastest release addresses several bugs encountered by the SUAVE community. It also contains improvements to our medium-fidelity and semi-emperical analysis methods. We suggest you upgrade to take advantage of these changes.

The big new features for version 2.3 are:

  • Updates to the native Vortex Lattice Method
  • Propeller-wing interaction modeling
  • Integrated FLOPS and Raymer aircraft weight estimation methods
  • Improvements to eVTOL networks
  • New constant-speed Internal Combustion Engine network
  • Lift-trimmed single point segments
  • Optimized range and endurance speeds for propeller aircraft
  • More regressions testing to support our Verification and Validation efforts

SUAVE 2.3, under the tree!


Download SUAVE 2.3

Merry Christmas,

The SUAVE Team

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SUAVE is maintained by the Aerospace Design Lab in the Department of Aeronautics and Astronautics at Stanford University and is released under an open-source license (LGPL v2.1). This list is only used to disseminate important information and updates regarding our software. The development team respects your privacy, and should you wish, you can unsubscribe from our email list.