SUAVE: An Open-Source Environment Enabling Unconventional Vehicle Designs through Higher Fidelity

SUAVE is a conceptual level aircraft design environment that incorporates multiple information sources to analyze unconventional configurations. This work incorporates higherfidelity tools to build upon previous efforts where SUAVE analyzed and optimized several types of aircraft using low-fidelity methods. This is done in an automated way that incorporates three external programs. The first is OpenVSP, which is used for geometry creation, area calculation, and surface meshing. The second is Gmsh, which uses these surface meshes to create volume meshes. The third is SU2, which is used to run Euler CFD simulations. Wetted areas from OpenVSP and lift from SU2 is used to enhance SUAVE’s aerodynamic analyses. We present results for a verification case with the Onera M6 wing, then present mission results with a conventional narrow-body airliner, a supersonic jet, and a blended wing body.

[1]  Mengmeng Zhang,et al.  Towards a collaborative and integrated set of open tools for aircraft design , 2013 .

[2]  R. H. Liebeck,et al.  Design of the Blended-Wing-Body subsonic transport , 2002 .

[3]  J. Alonso,et al.  Multifidelity Conceptual Design and Optimization of Strut-Braced Wing Aircraft using Physics Based Methods , 2016 .

[4]  M. H. Straathof,et al.  Adjoint Optimization of a Wing Using the CSRT Method , 2011 .

[5]  Mark Lutz,et al.  Learning Python , 1999 .

[6]  J. Remacle,et al.  Gmsh: A 3‐D finite element mesh generator with built‐in pre‐ and post‐processing facilities , 2009 .

[7]  Gaël Varoquaux,et al.  Scikit-learn: Machine Learning in Python , 2011, J. Mach. Learn. Res..

[8]  Juan J. Alonso,et al.  SUAVE: An Open-Source Environment for Multi-Fidelity Conceptual Vehicle Design , 2015 .

[9]  Juan J. Alonso,et al.  SUAVE: An Open-Source Environment for Conceptual Vehicle Design and Optimization , 2016 .

[10]  Viktoria Schmitt,et al.  Pressure distributions on the ONERA M6 wing at transonic Mach numbers , 1979 .

[11]  Christophe Geuzaine,et al.  Gmsh: A 3‐D finite element mesh generator with built‐in pre‐ and post‐processing facilities , 2009 .

[12]  Peter Sturdza,et al.  A Rapid Geometry Engine for Preliminary Aircraft Design , 2006 .

[13]  Andrew S. Hahn,et al.  Vehicle Sketch Pad: a Parametric Geometry Modeler for Conceptual Aircraft Design , 2010 .

[14]  Joaquim R. R. A. Martins,et al.  GeoMACH: Geometry-Centric MDAO of Aircraft Configurations with High Fidelity , 2012 .

[15]  Rakesh K. Kapania,et al.  Reevaluating conceptual design fidelity: An efficient supersonic air vehicle design case , 2016 .