Potential Flow, Circular Loop. Neglecting viscosity for an air glow find VP, the radial acceleration a,, and the circulation I (m²/s) (eqn. 6.89) about the circular loop given by r = 5m, for the following: (a) rigid body fluid rotation with Ve=5r; (b) the potential free vortex given by Y = 5 In r; (c) for which case (s), a and /or/ b, can the pressure difference between the origin and any other point be determined using the Bernoulli equation? Note that for both flows, V, = 0. Ans OM: (a) 10² Pa/m; -10² m/s²; 10² m²/s; (b) 10¹ Pa/m; -10¹ m/s²; -10¹ m²/s y.

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Chapter5: Analysis Of Convection Heat Transfer
Section: Chapter Questions
Problem 5.8P
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Potential Flow, Circular Loop. Neglecting viscosity for an air glow find VP, the radial acceleration ar, and the
circulation I (m²/s) (eqn. 6.89) about the circular loop given by r = 5m, for the following: (a) rigid body fluid
rotation with V₁ = 5r; (b) the potential free vortex given by Y = 5 In r; (c) for which case (s), a and/or/b, can the
pressure difference between the origin and any other point be determined using the Bernoulli equation? Note that
for both flows, V, = 0. Ans OM: (a) 10² Pa/m; -10² m/s²; 10² m²/s; (b) 10-¹ Pa/m; -10¹ m/s²; -10¹ m²/s
y
→x
Transcribed Image Text:Potential Flow, Circular Loop. Neglecting viscosity for an air glow find VP, the radial acceleration ar, and the circulation I (m²/s) (eqn. 6.89) about the circular loop given by r = 5m, for the following: (a) rigid body fluid rotation with V₁ = 5r; (b) the potential free vortex given by Y = 5 In r; (c) for which case (s), a and/or/b, can the pressure difference between the origin and any other point be determined using the Bernoulli equation? Note that for both flows, V, = 0. Ans OM: (a) 10² Pa/m; -10² m/s²; 10² m²/s; (b) 10-¹ Pa/m; -10¹ m/s²; -10¹ m²/s y →x
Cauchy's
ΣF )
equation of motion : pDV/Dt =pg + VT (like pa
Newtonian viscous stress relations by the tensor relation :
Ti j = - pôij + µ[Əvj/əxi + əvi/axj]
where dij is the kroneker delta function (1 for i
=
T includes pressure and viscous surface forces.
into Cauchy's equation, and assume constant viscosity, to get the Navier-Stokes
vector eq'ns : pDV/Dt
Pg -vp + μ^2 V
the acceleration DV/Dt
av/at+ (VV)V, which
for steady state flow gives DV/Dt =(V.) V.
Because (VV) V is a non-linear term on the LHS of the N-S equation
Reynolds Number
RepVL/μ, a measure of the ratio of inertial to viscous forces.
: Patm
10^5
=
=
N
=
N
=
; pwater 1000; pair 1.2; μwater 10^-3 N s/m^2
; Hair 2 x 10^-5 N•s/m^2
; g 9.8 m/s^2
=
j; 0 for i j );
N
Transcribed Image Text:Cauchy's ΣF ) equation of motion : pDV/Dt =pg + VT (like pa Newtonian viscous stress relations by the tensor relation : Ti j = - pôij + µ[Əvj/əxi + əvi/axj] where dij is the kroneker delta function (1 for i = T includes pressure and viscous surface forces. into Cauchy's equation, and assume constant viscosity, to get the Navier-Stokes vector eq'ns : pDV/Dt Pg -vp + μ^2 V the acceleration DV/Dt av/at+ (VV)V, which for steady state flow gives DV/Dt =(V.) V. Because (VV) V is a non-linear term on the LHS of the N-S equation Reynolds Number RepVL/μ, a measure of the ratio of inertial to viscous forces. : Patm 10^5 = = N = N = ; pwater 1000; pair 1.2; μwater 10^-3 N s/m^2 ; Hair 2 x 10^-5 N•s/m^2 ; g 9.8 m/s^2 = j; 0 for i j ); N
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