1
GATE ME 2003
MCQ (Single Correct Answer)
+2
-0.6
A syringe with a frictionless plunger contains water and has at its end a $$100$$ $$mm$$ long needle of $$1$$ $$mm$$ diameter. The internal diameter of the syringe is $$10$$ $$mm.$$ Water density is $$1000\,\,kg/{m^3}.$$ . The plunger is pushed in at $$10$$ $$mm/s$$ and the water comes out as a jet. GATE ME 2003 Fluid Mechanics - Turbulent Flow Question 6 English

Neglect losses in the cylinder and assume fully developed laminar viscous flow throughout the needle; the Darcy friction factor is $${64/R_e}$$. Where $${R_e}$$ is the Reynolds number. Given that the viscosity of water is $$1.0 \times {10^{ - 3}}\,\,kg/m\,\,\,s,$$ the force $$F$$ in newtons required on the plunger is

A
$$0.13$$
B
$$0.16$$
C
$$0.3$$
D
$$4.4$$
2
GATE ME 2003
MCQ (Single Correct Answer)
+2
-0.6
In a counter flow heat exchanger, for the hot fluid the heat capacity $$= 2kJ/kg$$ $$K,$$ mass flow rate $$= 5 kg/s,$$ inlet temperature $$ = {150^ \circ }C$$, outlet temperature $$ = {100^ \circ }C$$. For the cold fluid, heat capacity $$= 4 kJ/kg$$ $$K,$$ mass flow rate $$= 10 kg/s,$$ inlet temperature=$$ = {20^ \circ }C$$. Neglecting heat transfer to the surroundings, the outlet temperature of the cold fluid in $$ = {^ \circ }C$$ is
A
$$7.5$$
B
$$32.5$$
C
$$45.5$$
D
$$70.0$$
3
GATE ME 2003
MCQ (Single Correct Answer)
+1
-0.3
A plate having $$10\,\,c{m^2}$$ area each side is hanging in the middle of a room of $$100\,\,{m^2}$$ total surface area. The plate temperature and emissivity are respectively $$800$$ $$K$$ and $$0.6.$$

The temperature and emissivity values for the surfaces of the room are $$300$$ $$K$$ and $$0.3$$ respectively. Boltzmannn constant $$\sigma = 5.67 \times {10^{ - 8}}\,\,W/{m^2}{K^4}.$$ The total heat loss from the two surfaces of the plate is

A
$$13.66$$ $$W$$
B
$$27.32$$ $$W$$
C
$$27.87$$ $$W$$
D
$$13.66$$ $$MW$$
4
GATE ME 2003
MCQ (Single Correct Answer)
+2
-0.6
Consider a laminar boundary layer over a heated flat plate. The free stream velocity is $${U_\infty }.$$ At some distance $$x$$ from the leading edge the velocity boundary layer thickness is $${\delta _v}$$ and the thermal boundary layer is $${\delta _r}.$$ If the Prandtl number is greater than $$1,$$ then
A
$${\delta _v} > {\delta _r}$$
B
$${\delta _r} > {\delta _v}$$
C
$${\delta _v} = {\delta _r} \sim \left( {{U_\infty }} \right)$$
D
$${\delta _v} = {\delta _r} \sim {x^{ - 1/2}}$$
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