Using Surface Sensitivity from Mesh Adjoint Solution for Transonic Wing Drag Reduction (AIAA 2016-0560)
Aerospace sciences meeting
01.01.2016
28 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Using Surface Sensitivity from Mesh Adjoint for Transonic Wing Drag Reduction
Online Contents | 2016
|AIAA 2001-0560 Determining Aerodynamic Loads Based on Optical Deformation Measurements
British Library Conference Proceedings | 2001
|Using Mesh Adjoint for Shock Bump Deployment and Optimisation on Transonic Wings (AIAA 2015-1488)
British Library Conference Proceedings | 2015
|