|COOKIES: By using this website you agree that we can place Google Analytics Cookies on your device for performance monitoring.|
Shock control on transonic wings by three-dimensional bumps.
If you have a question about this talk, please contact ROBERTA TRUPIANO.
Sandwiches provided at 13:00, seminar begins 13:15.
The aerodynamics of modern transport aircraft wings are characterised by the appearance of weak normal (or near-normal) shock waves, which lead to an additional drag component (wave drag) and the possibility of buffet – oscillatory shock motion caused by the interaction of regions of shock-induced and trailing-edge boundary layer separation. Both of these phenomena effectively limit the operational speed of the aircraft, and controlling them is therefore desirable. One method that has shown considerable promise is the ‘shock control bump’ (SCB). Although there have been extensive studies on SCB performance conducted in previous years, the details of the flow physics still require research to enable improved designs that are more robust to off-design conditions. The present work examines flow features of shock bumps through a combination of experimental and computational investigations, highlighting the connection between bump geometry and flow properties. The SCB is also shown to produce streamwise vortices capable of exerting a degree of direct boundary layer control, and the origin of this flow feature is investigated. This suggests the potential of the SCB of acting as a new class of ‘smart’ vortex generator that offsets the viscous penalty of vortex generation by reduction of other shock-related drag components.
This talk is part of the Fluid Mechanics (CUED) series.
This talk is included in these lists:
Note that ex-directory lists are not shown.
Other listsCambridge University Geographical Society Type the title of a new list here Centre of African Studies Occasional Talks
Other talksIgnite 2016 - Fast-tracking innovation to commercial reality DEMENTIA: What It Is and How It Might Affect You Don't multiply lightly: exploring how DNN depth interacts with HMM independence assumptions in hybrid HMM/DNN's used for ASR RECHARGE and REFOCUS R&D Management Conference - From Science to Society - Innovation and Value Creation Biomedical Engineering: problem solving using clinical and biomedical applications