Corkery, SJ and Babinsky, H and Harvey, JK () On the development and early observations from a towing tank-based transverse wing–gust encounter test . Holger Babinsky of University of Cambridge, Cambridge (Cam) with expertise in: Aeronautical Engineering, Mechanical Engineering and Aerospace. Professor Holger Babinsky. Do you feel there’s something UNNATURAL about a giant plane being held up by thin air? If so, you owe it to yourself to discover the.

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Babinsky, H and Yang, J-M and Takayama, K Animated visualization of shock wave flowfields for dynamic comparison between experiment and computational prediction.

He has co-edited, together with Prof. These cookies and any others in use are detailed in our site privacy and cookie policies and are integral to our web site.

Davidson, TSC and Babinsky, H Influence of transition on the flow downstream of normal shock wave—boundary layer interactions. May Each student submits two copies of Babinsku report plus an extra copy of their technical abstract, plus their log book or electronic equivalent to Group Centres by 4pm.

About research at Cambridge. His main areas of research are in the field of experimental aerodynamics and associated measurement techniques.

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Journal of Aircraft, We may use cookies to record some preference settings and to analyse how you use our web site. Babinsky, H Cover Illustration.

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Typical research projects revolve hopger applications such as Formula 1, micro-air vehicles flapping wingsvertical axis wind turbines, shock control for transonic wings and supersonic engine inlets. This includes shock control e. Titchener, N and Babinsky, H A review of the use of vortex generators for mitigating shock-induced separation.

Aerospace Science babinssky Technology, Yang, J-M and Babinsky, H and Takayama, K Holographic interferometric animation of shock diffraction and reflection using a highly repeatable shock tube.

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More recently, work has started to improve the efficiency of long-haul road haulage vehicles. Benek, JA and Suchyta, CJ and Babinsky, H The effect of wind tunnel size and shock strength on incident shock boundary layer interaction experiments. Drag reduction by shock and boundary layer control: We may also use external analysis systems which may set additional cookies to perform their analysis.

Journal of Fluid Mechanics. Babinsky, H and Edwards, JA Quantitative heat transfer measurements using liquid crystal thermographs in short duration hypersonic flow.

Babinsky, H and Edwards, JA On the incipient separation of a turbulent hypersonic boundary layer. Harvey, the only textbook dedicated to SBLIs. High Performance Computing in Science and Engineering ‘ My research is primarily experimental, although I do combine this with analytical methods and occasionally CFD. This Site Uses Cookies We may use cookies to record some preference settings and to analyse how you use our web site.

The IFS Symposium, — to — pp. Groups within the Division. We may also use external analysis systems which may set additional cookies to perform their analysis. Contact us Information provided by: Ogawa, H and Babinsky, H Evaluation of wave drag reduction by flow control. Davidson, TSC and Babinsky, H An investigation of interactions between normal shocks and transitional boundary layers.

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My main areas of research are in the field of experimental aerodynamics and associated measurement techniques. Babinsky, H Aerodynamic improvements of paraglider performance. I have read and understood this message. Professor Babinsky’s research is concerned with fundamental and applied aerodynamics with application babinsoy aeronautics, road vehicles and energy production. Notes on Numerical Fluid Mechanics, Coschignano, A and Babinsky, H and Sheaf, C and Platt, E Influence of near-leading edge curvature on the performance of aero-engine intake lips at high-incidence.

We may use cookies to record some preference settings and to analyse how you use our web babinskh. Advances in Simulation of Wing and Nacelle Stall: Babinsky, H and Edwards, JA Automatic liquid crystal thermography for transient heat transfer measurements in hypersonic flow. Cambridge Univ Holgee. Oorebeek, JM and Babinsky, H Flow physics of a normal-hole bled supersonic turbulent boundary layer.