Aerospace Engineering > GATE 2010 > Boundary Layer Theory
Consider an incompressible 2-D viscous flow over a curved surface. Let the pressure distribution
on the surface be p(s)=2+sin(π2+s)N/m2, where s is the distance along the curved surface
from the leading edge. The flow separates at
on the surface be p(s)=2+sin(π2+s)N/m2, where s is the distance along the curved surface
from the leading edge. The flow separates at
Correct : c
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