Outline - Motivation - Transition control using discrete roughness elements (DRE) - Subsonic Aircraft Roughness Glove Experiment (SARGE) - Crossflow transition in the absence of control - Effect of control - Concluding Remarks
Extending Swept-Wing Natural Laminar Flow Using Discrete Roughness Element
41st AIAA Fluid Dynamics Conference ; 2011 ; Honolulu, HI, US
Miscellaneous
No indication
English
Discrete-Roughness-Element-Enhanced Swept-Wing Natural Laminar Flow at High Reynolds Numbers
Online Contents | 2015
|Experiments on Discrete Roughness Element Technology for Swept-Wing Laminar Flow Control
AIAA | 2019
|