chapter i history of boundary layer theory introduction in this chapter in section 1 we explained the boundary layer concept due to prandtl 1904 in detail in section 2 we ...
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...Chapter i history of boundary layer theory introduction in this section we explained the concept due to prandtl detail gave major developments two dimensional consists for axial symmetrical flow made a survey three lastly defined some basic concepts which require our problems be discussed ii s was first person who introduced he mathematical formation equations complete navier stokes are elliptic differential while parabolic transition from type equation it is one fundamental consequences asymptotic transformation conceived by because certain aspects solution full lost foundation all modern fluid mechanics and aerodynamics have been clarified study its effects on general around body such as aircraft response atmospheric gust flutter phenomenon involving wing etc cases velocity components depends only space corordinates at same time component direction third co ordinate did not exist depend coordinates has so far hardly elaborated enormous difficulties associated with problem encountered...