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
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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
|Legacy Aircraft Drag Reduction (AIAA 2016-0535)
British Library Conference Proceedings | 2016
|