甘文彪
.Airframe/intake–exhaust integration design of flying wing using a multi-bump strategy:Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering,2016
.Design optimization of a three-dimensional diffusing S-duct using a modified SST turbulent model:Aerospace Science & Technology,2017
.Robust design of a conformal expansion nozzle with the inverse-design idea:Chinese Journal of Aeronautics,2018
.An Investigation of the Aerodynamic Performance for a Fuel Saving Double Channel Wing Configuration:Energies,2019
.An investigation of the aerodynamic performance for a propeller-aided lift-enhancing double wing configuration:Aerospace Science & Technology,2020
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