{"product_id":"experimental-investigation-of-turbulent-boundary-layer-with-uniform-blowing-at-moderate-and-high-reynolds-numbers-von-gazi-hasanuzzaman","title":"Experimental Investigation of Turbulent Boundary Layer with Uniform Blowing at Moderate and High Reynolds Numbers","description":"\u003cp\u003eExperimental investigation in turbulent boundary layer flows represents one of the canonical\u003c\/p\u003e\u003cp\u003egeometries of wall bounded shear flows. Utmost relevance of such experiments, however,\u003c\/p\u003e\u003cp\u003eis applied in the engineering applications in aerospace and marine industries. In\u003c\/p\u003e\u003cp\u003eparticular, continuous effort is being imparted to explore the underlying physics of the\u003c\/p\u003e\u003cp\u003eflow in order to develop models for numerical tools and to achieve flow control. Flow\u003c\/p\u003e\u003cp\u003econtrol experiments have been widely investigated since 1930¿s. Several flow control\u003c\/p\u003e\u003cp\u003etechnique has been explored and have shown potential benefit. But the choice of control\u003c\/p\u003e\u003cp\u003etechnique depends largely on the boundary condition and the type of application.\u003c\/p\u003e\u003cp\u003eHence, friction drag of subsonic transport aircraft is intended to be reduced within the\u003c\/p\u003e\u003cp\u003escope of this Ph. D. topic. Therefore, application of active control method such as microblowing\u003c\/p\u003e\u003cp\u003eeffect in the incompressible, zero pressure gradient turbulent boundary layer was\u003c\/p\u003e\u003cp\u003einvestigated. A series of experiments have been performed in two different wind tunnel\u003c\/p\u003e\u003cp\u003efacilities. Wind tunnel from Department of Aerodynamics and Fluid Mechanics (LAS)\u003c\/p\u003e\u003cp\u003ewas used for the measurements for moderate Reynolds number range in co-operation\u003c\/p\u003e\u003cp\u003ewith the wind tunnel from Laboratoire de M¿ecanique de Feiret Lille for large Reynolds\u003c\/p\u003e\u003cp\u003enumber range. Measurements are conducted with the help of state-of-the-art techniques\u003c\/p\u003e\u003cp\u003esuch as Laser Doppler Anemometry, Particle Image Velocimetry and electronic pressure\u003c\/p\u003e\u003cp\u003esensors.\u003c\/p\u003e\u003cdiv class=\"aw-variant-hidden-subtitle-div\" id=\"aw-variant-subtitle-9783736975583\"\u003e\u003ch3\u003e\u003c\/h3\u003e\u003c\/div\u003e","brand":"Autorenwelt Shop","offers":[{"title":"Softcover - 9783736975583","offer_id":47274939121989,"sku":"9783736975583","price":53.88,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0940\/0622\/files\/aa0ad72d-799f-451c-b889-453fce5d019b.jpg?v=1776494228","url":"https:\/\/shop.autorenwelt.de\/products\/experimental-investigation-of-turbulent-boundary-layer-with-uniform-blowing-at-moderate-and-high-reynolds-numbers-von-gazi-hasanuzzaman","provider":"Autorenwelt Shop","version":"1.0","type":"link"}