Aeronautical Engineering/principle of flight

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Question
Respected sir ,


            please explain about boundry layer sepration?.  

Answer
Fluid flow along a duct or over a surface will be retarded at the wall by viscosity.  The thin layer of retarded flow is the boundary layer, which of course has the least momentum adjacent to the wall.  If a streamwise pressure gradient develops along the wall, such as will occur in a diffuser or on a curved wall that is curving away from the flow, the flow along the wall will separate from the wall if it does not have enough momentum to overcome the pressure gradient.  By separation, we mean that the streamlines will diverge away from the surface.  In the separated region, backflow and turbulence will fill the void.

Aeronautical Engineering

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Paul Soderman

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Aeronautics, Fluid Mechanics, Aeroacoustics, Noise Control, Muffler Design, Wind Tunnel Research.... I know nothing about India - do not ask about schools, jobs, application requirements, career choices, etc. for India. Please, no text message verbiage; I prefer full words in full sentences. Thanks.

Experience

38 years as research engineer at NASA

Publications
AIAA, NASA

Education/Credentials
B.S. and M.S. Aeronautical Engineering - U. of Washington Graduate work Standford U.

Awards and Honors
AIAA Associate Fellow (American Institute of Aeronautics and Astronautics)

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