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Fluid Mechanics

29 Questions
GATE→2026→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q1
MCQ[1 Mark]
A steady incompressible laminar flow passes through a 90∘90^{\circ} tube bend placed on a horizontal surface. In horizontal diametric plane, two pressure taps PiP_{i} and PoP_{o} are provided across the cross-section at inner and outer walls of the bend, respectively. Which one of the following options is correct?
GATE→2026→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q2
MCQ[1 Mark]
An ideal gas passes isothermally through a long horizontal uniform cross-section pipe under steady flow. Consider that the pressure gradient in the pipe is sufficient for a finite change in the density of the gas. If the flow of the gas is purely pressure driven and subsonic throughout, then the average flow velocity
GATE→2026→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q3
MCQ[1 Mark]
Bernoulli's equation CANNOT be applied between
Figure for Question 3
GATE→2026→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q4
MCQ[1 Mark]
A hydraulic crane supports a mass of 500 kg500~kg with its piston-cylinder actuator, inclined at 60∘60^{\circ} with horizontal, as shown in the figure below. The diameter of the piston is 30 cm30~cm and gravitational acceleration is 10 m/s210~m/s^{2}. Neglecting mass of the piston, the reading of the pressure gage in kPa (gage) is
Figure for Question 4
GATE→2026→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q5
NAT[2 Marks]
Water with a density of 1000 kg/m31000~kg/m^{3} comes out of an industrial condenser through a horizontal pipe of 15 cm15~cm radius at the flow rate of 4.5 m3/min4.5~m^{3}/min. The outlet of the pipe is connected to a coaxial diffuser of 0.5 m0.5~m length using a flange to raise the pressure of water to atmospheric condition without any backflow. The inner radius (rr, in mm) of the diffuser cross-section is expressed as r=0.15+0.4 x2r=0.15+0.4~x^{2} where, xx represents the axial distance of the diffuser in m, from its inlet. Considering frictionless flow, the magnitude of the force exerted by the diffuser on the flange is ____ N (rounded off to 2 decimal places).
GATE→2025→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q6
MCQ[1 Mark]
Consider two identical tanks with a bottom hole of diameter dd. One tank is filled with water and the other tank is filled with engine oil. The height of the fluid column hh is same in both the cases. The fluid exit velocity in the two tanks are V1V_{1} and V2V_{2}. Neglecting all losses, which one of the following options is correct?
Figure for Question 6
GATE→2025→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q7
MCQ[1 Mark]
In a laboratory experiment using a scaled down model to measure scour at a bridge pier, the Froude number is important. The ratio of the prototype length to the model length is 100100. If the velocity of the model is 1 m s−11~m~s^{-1}, the velocity (in m s−1m~s^{-1}) of the prototype is
GATE→2025→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q8
MSQ[2 Marks]
For a fully-developed pipe flow, which of the following options is/are correct?
GATE→2025→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q9
NAT[2 Marks]
A pitot tube connected to a U-tube mercury manometer measures the speed of air flowing in the wind tunnel as shown in the figure below. The density of air is 1.23 kg m−31.23~kg~m^{-3} while the density of water is 1000 kg m−31000~kg~m^{-3}. For the manometer reading of h=30 mmh=30~mm of mercury, the speed of air in the wind tunnel is ____ m s−1m~s^{-1} (rounded off to 1 decimal place).\nAssume: Specific gravity of mercury =13.6=13.6, Acceleration due to gravity =10 m s−2=10~m~s^{-2}
Figure for Question 9
GATE→2025→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q10
NAT[2 Marks]
Consider a velocity field V⃗=3zi^+0j^+Cxk^\vec{V}=3z\hat{i}+0\hat{j}+Cx\hat{k}, where CC is a constant. If the flow is irrotational, the value of CC is ____ (rounded off to 1 decimal place).
GATE→2024→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q11
MCQ[1 Mark]
The velocity field of a two-dimensional, incompressible flow is given by V⃗=2 sinh⁡xi^+v(x,y)j^\vec{V}=2~\sinh x\hat{i}+v(x,y)\hat{j}\nwhere i^\hat{i} and j^\hat{j} denote the unit vectors in xx and yy directions, respectively. If v(x,0)=cosh⁡xv(x,0)=\cosh x, then v(0,−1)v(0,-1) is
GATE→2024→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q12
MCQ[2 Marks]
In the pipe network shown in the figure, all pipes have the same cross-section and can be assumed to have the same friction factor. The pipes connecting points W, N, and S with point J have an equal length L. The pipe connecting points J and E has a length 10L. The pressures at the ends N, E, and S are equal. The flow rate in the pipe connecting W and J is Q. Assume that the fluid flow is steady, incompressible, and the pressure losses at the pipe entrance and junction are negligible. Consider the following statements:\nI: The flow rate in pipe connecting J and E is Q/21.\nII: The pressure difference between J and N is equal to the pressure difference between J and E.\nWhich one of the following options is CORRECT?
Figure for Question 12
GATE→2024→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q13
MSQ[2 Marks]
Steady, compressible flow of air takes place through an adiabatic converging-diverging nozzle, as shown in the figure. For a particular value of pressure difference across the nozzle, a stationary normal shock wave forms in the diverging section of the nozzle. If E and F denote the flow conditions just upstream and downstream of the normal shock, respectively, which of the following statement(s) is/are TRUE?
Figure for Question 13
GATE→2024→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q14
NAT[2 Marks]
A liquid fills a horizontal capillary tube whose one end is dipped in a large pool of the liquid. Experiments show that the distance LL travelled by the liquid meniscus in time tt is given by L=kγaRbμctL=k\gamma^{a}R^{b}\mu^{c}\sqrt{t}\nwhere γ\gamma is the surface tension, RR is the inner radius of the capillary, and μ\mu is the dynamic viscosity of the liquid. If kk is a dimensionless constant, then the value of aa is ____ (rounded off to 1 decimal place).
GATE→2023→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q15
MCQ[1 Mark]
Air (density =1.2 kg/m3=1.2~kg/m^{3}, kinematic viscosity =1.5×10−5m2/s=1.5\times 10^{-5}m^{2}/s) flows over a flat plate with a free-stream velocity of 2 m/s2~m/s. The wall shear stress at a location 15 mm15~mm from the leading edge is τw\tau_{w}. What is the wall shear stress at a location 30 mm30~mm from the leading edge?
GATE→2023→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q16
MCQ[1 Mark]
Consider an isentropic flow of air (ratio of specific heats =1.4=1.4) through a duct as shown in the figure. The variations in the flow across the cross-section are negligible. The flow conditions at Location 1 are given as follows: P1=100 kPaP_{1}=100~kPa, ρ1=1.2 kg/m3\rho_{1}=1.2~kg/m^{3}, u1=400 m/su_{1}=400~m/s\nThe duct cross-sectional area at Location 2 is given by A2=2A1A_{2}=2A_{1}, where A1A_{1} denotes the duct cross-sectional area at Location 1. Which one of the given statements about the velocity u2u_{2} and pressure P2P_{2} at Location 2 is TRUE?
Figure for Question 16
GATE→2023→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q17
NAT[2 Marks]
The velocity field of a certain two-dimensional flow is given by V⃗(x,y)=k(xi^−yj^)\vec{V}(x,y)=k(x\hat{i}-y\hat{j})\nwhere k=2 s−1k=2~s^{-1}. The coordinates xx and yy are in meters. Assume gravitational effects to be negligible.\nIf the density of the fluid is 1000 kg/m31000~kg/m^{3} and the pressure at the origin is 100 kPa100~kPa, the pressure at the location (2 m,2 m)(2~m, 2~m) is ____ kPa. (Answer in integer)
GATE→2023→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q18
NAT[2 Marks]
Consider a unidirectional fluid flow with the velocity field given by V(x,y,z,t)=u(x,t)i^V(x,y,z,t)=u(x,t)\hat{i}\nwhere u(0,t)=1u(0,t)=1. If the spatially homogeneous density field varies with time tt as ρ(t)=1+0.2e−t\rho(t)=1+0.2e^{-t}\nthe value of u(2,1)u(2,1) is ____ (Rounded off to two decimal places)\nAssume all quantities to be dimensionless.
GATE→2023→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q19
NAT[2 Marks]
The figure shows two fluids held by a hinged gate. The atmospheric pressure is Pa=100 kPaP_{a}=100~kPa. The moment per unit width about the base of the hinge is ____ kNm/m. (Rounded off to one decimal place)\nTake the acceleration due to gravity to be g=9.8 m/s2g=9.8~m/s^{2}.
Figure for Question 19
GATE→2023→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q20
NAT[2 Marks]
An explosion at time t=0t=0 releases energy EE at the origin in space filled with a gas of density ρ\rho. Subsequently, a hemispherical blast wave propagates radially outwards as shown in the figure. Let RR denote the radius of the front of the hemispherical blast wave. The radius RR follows the relationship R=k taEbρcR=k~t^{a}E^{b}\rho^{c} where kk is a dimensionless constant. The value of exponent aa is ____ (Rounded off to one decimal place)
Figure for Question 20
GATE→2022→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q21
MCQ[1 Mark]
A tiny temperature probe is fully immersed in a flowing fluid and is moving with zero relative velocity with respect to the fluid. The velocity field in the fluid is 𝑽ሬ⃗= (2𝑥)ଙ̂ + (𝑦+ 3𝑡)ଚ̂, and the temperature field in the fluid is 𝑇= 2𝑥ଶ+ 𝑥𝑦+ 4𝑡, where x and y are the spatial coordinates, and t is the time. The time rate of change of temperature recorded by the probe at (𝑥= 1, 𝑦= 1, 𝑡= 1) is _______. (A) 4 (B) 0 (C) 18 (D) 14
GATE→2022→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q22
MCQ[1 Mark]
In the following two-dimensional momentum equation for natural convection over a surface immersed in a quiescent fluid at temperature 𝑇ஶ (𝑔 is the gravitational acceleration, 𝛽 is the volumetric thermal expansion coefficient, 𝝂 is the kinematic viscosity, 𝑢 and 𝑣 are the velocities in 𝑥 and 𝑦 directions, respectively, and T is the temperature) 𝑢 డ௨ డ௫+ 𝑣 డ௨ డ௬= 𝑔𝛽(𝑇−𝑇ஶ) + 𝝂 డమ௨ డ௬మ , the term 𝑔𝛽(𝑇−𝑇ஶ) represents (A) Ratio of inertial force to viscous force. (B) Ratio of buoyancy force to viscous force. (C) Viscous force per unit mass. (D) Buoyancy force per unit mass.
GATE→2022→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q23
MSQ[1 Mark]
The figure shows a purely convergent nozzle with a steady, inviscid compressible flow of an ideal gas with constant thermophysical properties operating under choked condition. The exit plane shown in the figure is located within the nozzle. If the inlet pressure (P0) is increased while keeping the back pressure (Pback) unchanged, which of the following statements is/are true? (A) Mass flow rate through the nozzle will remain unchanged. (B) Mach number at the exit plane of the nozzle will remain unchanged at unity. (C) Mass flow rate through the nozzle will increase. (D) Mach number at the exit plane of the nozzle will become more than unity.
Figure for Question 23
GATE→2022→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q24
MCQ[2 Marks]
A solid spherical bead of lead (uniform density = 11000 kg/m3) of diameter d = 0.1 mm sinks with a constant velocity V in a large stagnant pool of a liquid (dynamic viscosity = 1.1 × 10ିଷ kg∙m∙s). The coefficient of drag is given by 𝑐஽= ଶସ ୖୣ, where the Reynolds number (Re) is defined on the basis of the diameter of the bead. The drag force acting on the bead is expressed as 𝐷= (𝑐஽)(0.5𝜌𝑉ଶ) ቀ గௗమ ସቁ, where ρ is the density of the liquid. Neglect the buoyancy force. Using 𝑔= 10 m/s2, the velocity V is __________ m/s. (A) 1 24 (B) 1 6 (C) 1 18 (D) 1 12
GATE→2022→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q25
MCQ[2 Marks]
Consider steady, one-dimensional compressible flow of a gas in a pipe of diameter 1 m. At one location in the pipe, the density and velocity are 1 kg/m3 and 100 m/s, respectively. At a downstream location in the pipe, the velocity is 170 m/s. If the pressure drop between these two locations is 10 kPa, the force exerted by the gas on the pipe between these two locations is ____________ N. (A) 350𝜋ଶ (B) 750π (C) 1000π (D) 3000
GATE→2022→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q26
NAT[2 Marks]
In a steam power plant based on Rankine cycle, steam is initially expanded in a high-pressure turbine. The steam is then reheated in a reheater and finally expanded in a low-pressure turbine. The expansion work in the high-pressure turbine is 400 kJ/kg and in the low-pressure turbine is 850 kJ/kg, whereas the pump work is 15 kJ/kg. If the cycle efficiency is 32%, the heat rejected in the condenser is ________ kJ/kg (round off to 2 decimal places).
GATE→2022→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q27
NAT[2 Marks]
A steady two-dimensional flow field is specified by the stream function 𝜓= 𝑘𝑥ଷ𝑦, where 𝑥 and 𝑦 are in meter and the constant 𝑘 = 1 ms. The magnitude of acceleration at a point (x, y) = (1 m, 1 m) is ________ m/s2 (round off to 2 decimal places).
GATE→2022→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q28
NAT[2 Marks]
Consider a solid slab (thermal conductivity, k = 10 W∙m∙K) with thickness 0.2 m and of infinite extent in the other two directions as shown in the figure. Surface 2, at 300 K, is exposed to a fluid flow at a free stream temperature (T∞) of 293 K, with a convective heat transfer coefficient (h) of 100 W∙m∙K. Surface 2 is opaque, diffuse and gray with an emissivity () of 0.5 and exchanges heat by radiation with very large surroundings at 0 K. Radiative heat transfer inside the solid slab is neglected. The Stefan-Boltzmann constant is 5.67×108 W∙m∙K. The temperature T1 of Surface 1 of the slab, under steady-state conditions, is _________ K (round off to the nearest integer).
Figure for Question 28
GATE→2022→Fluid Mechanics and Thermal Sciences→Fluid Mechanics
Q29
NAT[2 Marks]
During open-heart surgery, a patient’s blood is cooled down to 25 C from 37 C using a concentric tube counter-flow heat exchanger. Water enters the heat exchanger at 4 C and leaves at 18 C. Blood flow rate during the surgery is 5 L/minute. Use the following fluid properties: Fluid Density (kg/m3) Specific heat (J/kg-K) Blood 1050 3740 Water 1000 4200 Effectiveness of the heat exchanger is _________ (round off to 2 decimal places).

Heat Transfer

23 Questions
GATE→2026→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q30
MCQ[1 Mark]
A quiescent fluid at temperature T3T_{3} is confined between two vertical parallel plates. While plate 1 is kept at temperature T1T_{1} and plate 2 is maintained at temperature T2T_{2}, a velocity profile between the plates, as shown in the figure below, is generated due to heat transfer. Which one of the following options shows the correct relations among T1T_{1}, T2T_{2}, and T3T_{3}?
Figure for Question 30
GATE→2026→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q31
NAT[1 Mark]
A sphere of radius 5 mm5~mm is initially in equilibrium at 400∘C400^{\circ}C in a furnace. It is suddenly removed from the furnace and dipped in a well-stirred water bath at 20∘C20^{\circ}C, with a convection heat transfer coefficient of 500 W/(m2K)500~W/(m^{2}K). For the given range of temperatures, the thermophysical properties of the material of the sphere are: density ρ=3000 kg/m3\rho=3000~kg/m^{3}, thermal conductivity k=10 W/(m K)k=10~W/(m~K), and specific heat c=1000 J/(kg K)c=1000~J/(kg~K). Neglecting radiation heat transfer, the time required for the centre of the sphere to cool from 400∘C400^{\circ}C to 50∘C50^{\circ}C is ____ seconds (rounded off to 2 decimal places).
Figure for Question 31
GATE→2026→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q32
MCQ[2 Marks]
A very long fin of a uniform square cross-section is replaced by another very long fin of a uniform circular cross-section of the same material. Assume uniform and identical heat transfer coefficient for both the fins. If the diameter of ket circular fin is equal to the side length of the square fin, then the ratio of heat transfer rates before and after the replacement is
GATE→2026→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q33
NAT[2 Marks]
Two rectangular surfaces both having 1 m21~m^{2} area are placed perpendicular to each other with a common edge. One surface is hot, having a temperature of 1000 K1000~K and emissivity of 0.40.4, while the other is insulated and in radiant balance with a large surrounding room at 300 K300~K. If the fraction of radiation leaving the hot surface which reaches the cold surface is 0.20.2, then the equivalent overall resistance for the radiation heat loss from the hot surface is ____ m−2m^{-2} (rounded off to 2 decimal places).
GATE→2026→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q34
NAT[2 Marks]
Convective heat transfer coefficients for Fluid 1 and Fluid 2 in a heat exchanger, as shown in the figure below, are 50 W/(m2K)50~W/(m^{2}K) and 80 W/(m2K)80~W/(m^{2}K), respectively. The inner tube is made of a material which has a thermal conductivity 386 W/(m K)386~W/(m~K) for the given range of temperatures in the heat exchanger. The length of the heat exchanging surface, the inside radius of the inner tube, and thickness of the inner tube are 1 m1~m, 10 mm10~mm, and 1 mm1~mm, respectively. Considering no heat exchange between the outer tube and the surrounding, the heat transfer rate for the heat exchanger is ____ W (rounded off to 1 decimal place).
Figure for Question 34
GATE→2025→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q35
MCQ[1 Mark]
Let a spherical block of ice at −7∘C-7^{\circ}C be exposed to atmospheric air at 30∘C30^{\circ}C with the gravitational direction as shown in the figure below. What will be the overall direction of air flow in this situation?
Figure for Question 35
GATE→2025→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q36
NAT[2 Marks]
Consider a cylindrical furnace of 5 m5~m diameter and 5 m5~m length with bottom, top and curved surfaces maintained at uniform temperatures of 800 K800~K, 1500 K1500~K and 500 K500~K, respectively. The view factor between the bottom and top surfaces, F12F_{12} is 0.20.2. The magnitude of net radiation heat transfer rate between the bottom surface and the curved surface is ____ kW (rounded off to 1 decimal place).\nAll surfaces of the furnace can be assumed as black.\nThe Stefan-Boltzmann constant, σ=5.67×10−8 W m−2K−4\sigma=5.67\times 10^{-8}~W~m^{-2}K^{-4}.
Figure for Question 36
GATE→2025→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q37
NAT[2 Marks]
Water enters a tube of diameter, D=60 mmD=60~mm with mass flow rate of 0.01 kg s−10.01~kg~s^{-1} as shown in the figure below. The inlet mean temperature is Tm,i=293 KT_{m,i}=293~K and the uniform heat flux at the surface of the tube is 2000 W m−22000~W~m^{-2}. For the exit mean temperature of Tm,o=353 KT_{m,o}=353~K, the length of the tube, LL is ____ m (rounded off to 1 decimal place).\nUse the specific heat of water as 4181 J kg−1K−14181~J~kg^{-1}K^{-1}.
Figure for Question 37
GATE→2024→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q38
MCQ[1 Mark]
A plane, solid slab of thickness L, shown in the figure, has thermal conductivity kk that varies with the spatial coordinate xx as k=A+Bxk=A+Bx, where AA and BB are positive constants (A>0,B>0A>0, B>0). The slab walls are maintained at fixed temperatures of T(x=0)=0T(x=0)=0 and T(x=L)=T0>0T(x=L)=T_{0}>0. The slab has no internal heat sources. Considering one-dimensional heat transfer, which one of the following plots qualitatively depicts the steady-state temperature distribution within the slab?
Figure for Question 38
GATE→2024→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q39
MCQ[1 Mark]
Consider incompressible laminar flow over a flat plate with freestream velocity of u∞u_{\infty}. The Nusselt number corresponding to this flow velocity is Nu1Nu_{1}. If the freestream velocity is doubled, the Nusselt number changes to Nu2Nu_{2}. Choose the correct option for Nu2/Nu1Nu_{2}/Nu_{1}.
GATE→2024→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q40
MCQ[1 Mark]
Consider a hydrodynamically fully developed laminar flow through a circular pipe with the flow along the axis (i.e., zz direction). In the following statements, TT is the temperature of the fluid, TwT_{w} is the wall temperature and TmT_{m} is the bulk mean temperature of the fluid. Which one of the following statements is TRUE? [Note: Official Key marked this as MTA (Marks To All)]
GATE→2024→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q41
NAT[2 Marks]
Consider a slab of 20 mm20~mm thickness. There is a uniform heat generation of q˙=100 MW/m3\dot{q}=100~MW/m^{3} inside the slab. The left and right faces of the slab are maintained at 150∘C150^{\circ}C and 110∘C110^{\circ}C, respectively. The plate has a constant thermal conductivity of 200 W/(m⋅K)200~W/(m \cdot K). Considering a 1-D steady state heat conduction, the location of the maximum temperature from the left face will be at ____ mm (answer in integer).
Figure for Question 41
GATE→2024→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q42
NAT[2 Marks]
A condenser is used as a heat exchanger in a large steam power plant in which steam is condensed to liquid water. The condenser is a shell and tube heat exchanger which consists of 1 shell and 20,000 tubes. Water flows through each of the tubes at a rate of 1 kg/s1~kg/s with an inlet temperature of 30∘C30^{\circ}C. The steam in the condenser shell condenses at the rate of 430 kg/s430~kg/s at a temperature of 50∘C50^{\circ}C. If the heat of vaporization is 2.326 MJ/kg2.326~MJ/kg and specific heat of water is 4 kJ/(kg⋅K)4~kJ/(kg \cdot K), the effectiveness of the heat exchanger is ____ (rounded off to 3 decimal places).
GATE→2024→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q43
NAT[2 Marks]
Consider a hemispherical furnace of diameter D=6 mD=6~m with a flat base. The dome of the furnace has an emissivity of 0.70.7 and the flat base is a blackbody. The base and the dome are maintained at uniform temperature of 300 K300~K and 1200 K1200~K, respectively. Under steady state conditions, the rate of radiation heat transfer from the dome to the base is ____ kW (rounded off to 1 decimal place).\nUse Stefan-Boltzmann constant =5.67×10−8 W/(m2K4)=5.67\times 10^{-8}~W/(m^{2}K^{4})
Figure for Question 43
GATE→2023→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q44
MCQ[1 Mark]
Consider incompressible laminar flow of a constant property Newtonian fluid in an isothermal circular tube. The flow is steady with fully-developed temperature and velocity profiles. The Nusselt number for this flow depends on
GATE→2023→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q45
MSQ[1 Mark]
Consider a laterally insulated rod of length L and constant thermal conductivity. Assuming one-dimensional heat conduction in the rod, which of the following steady-state temperature profile(s) can occur without internal heat generation?
Figure for Question 45
GATE→2023→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q46
NAT[1 Mark]
Consider a counter-flow heat exchanger with the inlet temperatures of two fluids (1 and 2) being T1,in=300 KT_{1,in}=300~K and T2,in=350 KT_{2,in}=350~K. The heat capacity rates of the two fluids are C1=1000 W/KC_{1}=1000~W/K and C2=400 W/KC_{2}=400~W/K and the effectiveness of the heat exchanger is 0.50.5. The actual heat transfer rate is ____ kW. (Answer in integer)
GATE→2023→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q47
MCQ[2 Marks]
A cylindrical rod of length hh and diameter dd is placed inside a cubic enclosure of side length LL. S denotes the inner surface of the cube. The view-factor FS−SF_{S-S} is
GATE→2023→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q48
MSQ[2 Marks]
A very large metal plate of thickness d and thermal conductivity k is cooled by a stream of air at temperature T∞=300 KT_{\infty}=300~K with a heat transfer coefficient h, as shown in the figure. The centerline temperature of the plate is TPT_{P}. In which of the following case(s) can the lumped parameter model be used to study the heat transfer in the metal plate?
Figure for Question 48
GATE→2022→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q49
MCQ[2 Marks]
In Fe-Fe3C phase diagram, the eutectoid composition is 0.8 weight % of carbon at 725 ºC. The maximum solubility of carbon in α-ferrite phase is 0.025 weight % of carbon. A steel sample, having no other alloying element except 0.5 weight % of carbon, is slowly cooled from 1000 ºC to room temperature. The fraction of pro-eutectoid α-ferrite in the above steel sample at room temperature is (A) 0.387 (B) 0.864 (C) 0.475 (D) 0.775
GATE→2022→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q50
NAT[2 Marks]
Two mild steel plates of similar thickness, in butt-joint configuration, are welded by gas tungsten arc welding process using the following welding parameters. Welding voltage 20 V Welding current 150 A Welding speed 5 mm/s A filler wire of the same mild steel material having 3 mm diameter is used in this welding process. The filler wire feed rate is selected such that the final weld bead is composed of 60% volume of filler and 40% volume of plate material. The heat required to melt the mild steel material is 10 J/mm3. The heat transfer factor is 0.7 and melting factor is 0.6. The feed rate of the filler wire is __________ mm/s (round off to one decimal place).
GATE→2022→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q51
NAT[2 Marks]
Consider a one-dimensional steady heat conduction process through a solid slab of thickness 0.1 m. The higher temperature side A has a surface temperature of 80 C, and the heat transfer rate per unit area to low temperature side B is 4.5 kW/m2. The thermal conductivity of the slab is 15 W/m.K. The rate of entropy generation per unit area during the heat transfer process is ________ W/m2.K (round off to 2 decimal places).
GATE→2022→Fluid Mechanics and Thermal Sciences→Heat Transfer
Q52
NAT[2 Marks]
An engine running on an air standard Otto cycle has a displacement volume 250 cm3 and a clearance volume 35.7 cm3. The pressure and temperature at the beginning of the compression process are 100 kPa and 300 K, respectively. Heat transfer during constant-volume heat addition process is 800 kJ/kg. The specific heat at constant volume is 0.718 kJ/kg.K and the ratio of specific heats at constant pressure and constant volume is 1.4. Assume the specific heats to remain constant during the cycle. The maximum pressure in the cycle is ______ kPa (round off to the nearest integer).

Thermodynamics

16 Questions
GATE→2026→Fluid Mechanics and Thermal Sciences→Thermodynamics
Q53
MCQ[1 Mark]
For an ideal gas, starting from state point 1, two different processes take place. The corresponding final states in these two processes are 2 and 3, lying on same isotherm. If P and h represent pressure and enthalpy, respectively, then which one of the following options is correct?
GATE→2026→Fluid Mechanics and Thermal Sciences→Thermodynamics
Q54
MCQ[1 Mark]
For the isothermal expansion of an ideal gas in a piston cylinder system, the net heat supplied during the process is equal to the net work. Which one of the following statements is correct for the given process?
GATE→2026→Fluid Mechanics and Thermal Sciences→Thermodynamics
Q55
NAT[2 Marks]
A liquid comes out of the reactor of a chemical plant at 250∘C250^{\circ}C temperature with a flow rate of 100 LPM100~LPM. The ambient temperature is 25∘C25^{\circ}C. Density and specific heat of the liquid remain constant at 1000 kg/m31000~kg/m^{3} and 4.18 kJ/(kg K)4.18~kJ/(kg~K), respectively, for the given range of temperature. The rate of exergy associated with the hot liquid stream at the exit of the plant is ____ kW (rounded off to 2 decimal places).
GATE→2026→Fluid Mechanics and Thermal Sciences→Thermodynamics
Q56
NAT[2 Marks]
A rigid closed vertical cylindrical vessel of 15 cm15~cm diameter contains 5 kg5~kg water at 80∘C80^{\circ}C with 10%10\% quality. The water is heated till its temperature reaches 130∘C130^{\circ}C. Considering only a horizontal separated interface between liquid and vapor, the dip in the liquid level after heating process is ____ cm (rounded off to 2 decimal places).
GATE→2025→Fluid Mechanics and Thermal Sciences→Thermodynamics
Q57
MCQ[1 Mark]
Air inside a rigid, thermally-insulated tank undergoes stirring as shown in the figure below. Which one of the following options is correct?
Figure for Question 57
GATE→2025→Fluid Mechanics and Thermal Sciences→Thermodynamics
Q58
NAT[2 Marks]
A thermodynamically closed system contains 1 kg1~kg of hydrogen. The system undergoes a reversible polytropic process with polytropic index 1.31.3. The work output during the process is 400 kJ400~kJ. During the process, hydrogen behaves as an ideal gas with constant specific heats. The absolute value of heat transfer during the process is ____ kJ (rounded off to 1 decimal place).\nSpecific heat of hydrogen at constant pressure =14.56 kJ kg−1K−1= 14.56~kJ~kg^{-1}K^{-1}\nSpecific heat of hydrogen at constant volume =10.4 kJ kg−1K−1= 10.4~kJ~kg^{-1}K^{-1}
GATE→2024→Fluid Mechanics and Thermal Sciences→Thermodynamics
Q59
MCQ[1 Mark]
A furnace can supply heat steadily at 1200 K1200~K at a rate of 24000 kJ/min24000~kJ/min. The maximum amount of power (in kW) that can be produced by using the heat supplied by this furnace in an environment at 300 K300~K is
GATE→2024→Fluid Mechanics and Thermal Sciences→Thermodynamics
Q60
MCQ[1 Mark]
Which one of the following statements regarding a Rankine cycle is FALSE?
GATE→2024→Fluid Mechanics and Thermal Sciences→Thermodynamics
Q61
NAT[2 Marks]
A piston-cylinder arrangement shown in the figure has a stop located 2 m2~m above the base. The cylinder initially contains air at 140 kPa140~kPa and 350∘C350^{\circ}C and the piston is resting in equilibrium at a position which is 1 m1~m above the stops (3 m3~m total height). The system is now cooled to the ambient temperature of 25∘C25^{\circ}C. Consider air to be an ideal gas with a value of gas constant R=0.287 kJ/(kg⋅K)R=0.287~kJ/(kg \cdot K).\nThe absolute value of specific work done during the process is ____ kJ/kg (rounded off to 1 decimal place).
Figure for Question 61
GATE→2024→Fluid Mechanics and Thermal Sciences→Thermodynamics
Q62
NAT[2 Marks]
A heat pump (H.P.) is driven by the work output of a heat engine (H.E.) as shown in the figure. The heat engine extracts 150 kJ150~kJ of heat from the source at 1000 K1000~K. The heat pump absorbs heat from the ambient at 280 K280~K and delivers heat to the room which is maintained at 300 K300~K. Considering the combined system to be ideal, the total amount of heat delivered to the room together by the heat engine and heat pump is ____ kJ (answer in integer).
Figure for Question 62
GATE→2023→Fluid Mechanics and Thermal Sciences→Thermodynamics
Q63
MCQ[1 Mark]
A heat engine extracts heat (QH)(Q_{H}) from a thermal reservoir at a temperature of 1000 K1000~K and rejects heat (QL)(Q_{L}) to a thermal reservoir at a temperature of 100 K100~K, while producing work (W). Which one of the combinations of [QH,QL and WQ_{H}, Q_{L} \text{ and } W] given is allowed?
GATE→2023→Fluid Mechanics and Thermal Sciences→Thermodynamics
Q64
MCQ[2 Marks]
Which one of the following statements is FALSE?
GATE→2023→Fluid Mechanics and Thermal Sciences→Thermodynamics
Q65
MCQ[2 Marks]
Consider a fully adiabatic piston-cylinder arrangement as shown in the figure. The piston is massless and cross-sectional area of the cylinder is A. The fluid inside the cylinder is air (considered as a perfect gas), with γ\gamma being the ratio of the specific heat at constant pressure to the specific heat at constant volume for air. The piston is initially located at a position L1L_{1}. The initial pressure of the air inside the cylinder is P1≫P0P_{1}\gg P_{0} where P0P_{0} is the atmospheric pressure. The stop S1S_{1} is instantaneously removed and the piston moves to the position L2L_{2}, where the equilibrium pressure of air inside the cylinder is P2≫P0P_{2}\gg P_{0}.\nWhat is the work done by the piston on the atmosphere during this process?
Figure for Question 65
GATE→2023→Fluid Mechanics and Thermal Sciences→Thermodynamics
Q66
NAT[2 Marks]
Consider a mixture of two ideal gases, X and Y, with molar masses M‾X=10 kg/kmol\overline{M}_{X}=10~kg/kmol and M‾Y=20 kg/kmol\overline{M}_{Y}=20~kg/kmol, respectively, in a container. The total pressure in the container is 100 kPa100~kPa, the total volume of the container is 10 m310~m^{3} and the temperature of the contents of the container is 300 K300~K. If the mass of gas-X in the container is 2 kg2~kg, then the mass of gas-Y in the container is ____ kg. (Rounded off to one decimal place)\nAssume that the universal gas constant is 8314 J⋅kmol−1K−18314~J \cdot kmol^{-1}K^{-1}.
GATE→2022→Fluid Mechanics and Thermal Sciences→Thermodynamics
Q67
MCQ[1 Mark]
The Clausius inequality holds good for (A) any process (B) any cycle (C) only reversible process (D) only reversible cycle
GATE→2022→Fluid Mechanics and Thermal Sciences→Thermodynamics
Q68
NAT[1 Mark]
A polytropic process is carried out from an initial pressure of 110 kPa and volume of 5 m3 to a final volume of 2.5 m3. The polytropic index is given by 𝑛= 1.2. The absolute value of the work done during the process is _______ kJ (round off to 2 decimal places).

Applications (Power Engineering, I.C. Engines, Refrigeration, Turbomachinery)

8 Questions
GATE→2026→Fluid Mechanics and Thermal Sciences→Applications (Power Engineering, I.C. Engines, Refrigeration, Turbomachinery)
Q69
MCQ[2 Marks]
For an ideal regenerative Rankine cycle, as shown in the figure below, which one of the following options is the correct representation of temperature-entropy (T-s) diagram?
Figure for Question 69
GATE→2026→Fluid Mechanics and Thermal Sciences→Applications (Power Engineering, I.C. Engines, Refrigeration, Turbomachinery)
Q70
NAT[2 Marks]
An inward flow reaction turbine, having an outer diameter of 1 m1~m, runs at 600 RPM600~RPM. The normal component of absolute velocity at the inlet is 10 m/s10~m/s. If the guide blade angle is 15∘15^{\circ}, then the inlet vane angle of the runner is ____ degree (rounded off to 1 decimal place).
Figure for Question 70
GATE→2025→Fluid Mechanics and Thermal Sciences→Applications (Power Engineering, I.C. Engines, Refrigeration, Turbomachinery)
Q71
MCQ[1 Mark]
In a psychrometric chart, one axis represents dry-bulb temperature. The axis, that is perpendicular to the dry-bulb temperature axis, represents
GATE→2025→Fluid Mechanics and Thermal Sciences→Applications (Power Engineering, I.C. Engines, Refrigeration, Turbomachinery)
Q72
NAT[1 Mark]
The thermal efficiency of an ideal air-standard Otto cycle is 0.50.5. The value of specific heat ratio of air is 1.41.4. The compression ratio of the cycle is ____ (rounded off to 1 decimal place).
GATE→2025→Fluid Mechanics and Thermal Sciences→Applications (Power Engineering, I.C. Engines, Refrigeration, Turbomachinery)
Q73
NAT[2 Marks]
A thermal power plant is running with no reheat or regeneration. The specific enthalpy and specific entropy of steam at the turbine inlet are 3344 kJ kg−13344~kJ~kg^{-1} and 6.5 kJ kg−1K−16.5~kJ~kg^{-1}K^{-1} respectively. The turbine isentropic efficiency is 0.90.9, and the mass flow rate of steam at the turbine inlet is 102 kg s−1102~kg~s^{-1}. The turbine power output is ____ MW (rounded off to 1 decimal place).
GATE→2025→Fluid Mechanics and Thermal Sciences→Applications (Power Engineering, I.C. Engines, Refrigeration, Turbomachinery)
Q74
NAT[2 Marks]
Consider a Pelton wheel of 1 m1~m diameter. The magnitude of relative velocity of water at the bucket inlet is same as the magnitude of relative velocity of water at the bucket exit. The absolute speed of water at the bucket inlet is 125.66 m s−1125.66~m~s^{-1}. For maximum power output from the Pelton wheel, the rpm of the Pelton wheel is ____ (rounded off to 1 decimal place).
GATE→2025→Fluid Mechanics and Thermal Sciences→Applications (Power Engineering, I.C. Engines, Refrigeration, Turbomachinery)
Q75
NAT[2 Marks]
A heat pump, operating in reversed Carnot cycle, maintains a steady air temperature of 300 K300~K inside an auditorium. The heat pump receives heat from the ambient air. The ambient air temperature is 280 K280~K. Heat loss from the auditorium is 15 kW15~kW. The power consumption of the heat pump is ____ kW (rounded off to 2 decimal places).
GATE→2024→Fluid Mechanics and Thermal Sciences→Applications (Power Engineering, I.C. Engines, Refrigeration, Turbomachinery)
Q76
NAT[2 Marks]
Consider an air-standard Brayton cycle with adiabatic compressor and turbine, and a regenerator, as shown in the figure. Air enters the compressor at 100 kPa100~kPa and 300 K300~K and exits the compressor at 600 kPa600~kPa and 550 K550~K. The air exits the combustion chamber at 1250 K1250~K and exits the adiabatic turbine at 100 kPa100~kPa and 800 K800~K. The exhaust air from the turbine is used to preheat the air in the regenerator. The exhaust air exits the regenerator (state 6) at 600 K600~K. There is no pressure drop across the regenerator and the combustion chamber. Also, there is no heat loss from the regenerator to the surroundings. The ratio of specific heats at constant pressure and volume is cp/cv=1.4c_{p}/c_{v}=1.4. The thermal efficiency of the cycle is ____ % (answer in integer).
Figure for Question 76