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Aerospace Engineering
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Aerodynamics
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Momentum Integral Equation
Momentum Integral Equation
An integrated form of the momentum equation across the boundary layer thickness
δ
\delta
δ
. It relates the drag force to the pressure gradient and the integral of the shear stress:
d
d
x
(
∫
0
δ
u
(
x
,
y
)
ρ
d
y
)
=
−
d
d
x
(
1
2
ρ
U
2
)
+
d
τ
w
d
x
\frac{d}{dx} (\int_0^\delta u(x,y) \rho dy) = -\frac{d}{dx} (\frac{1}{2}\rho U^2) + \frac{d\tau_w}{dx}
d
x
d
(
∫
0
δ
u
(
x
,
y
)
ρ
d
y
)
=
−
d
x
d
(
2
1
ρ
U
2
)
+
d
x
d
τ
w
.