Resilience
Proof resilience
Modulus of resilience
Toughness
A. Resilience
-100 MPa
250 MPa
300 MPa
400 MPa
Greater than
Less than
Equal to
None of these
Change
Do not change
Both (A) and (B)
None of these
Carnot cycle
Bell-Coleman cycle
Rankine cycle
Stirling cycle
Double
Half
Same
None of these
The material A is more ductile than material B
The material B is more ductile than material A
The ductility of material A and B is equal
The material A is brittle and material B is ductile
Vapour
Perfect gas
Air
Steam
Gauge pressure = Absolute pressure + Atmospheric pressure
Absolute pressure = Gauge pressure + Atmospheric pressure
Absolute pressure = Gauge pressure - Atmospheric pressure
Atmospheric pressure = Absolute pressure + Gauge pressure
30 kJ
54 kJ
84 kJ
114 kJ
Tensile stress
Compressive stress
Shear stress
Strain
Otto cycle is more efficient than Diesel cycle
Diesel cycle is more efficient than Otto cycle
Efficiency depends on other factors
Both Otto and Diesel cycles are equally efficient
Greater than Diesel cycle and less than Otto cycle
Less than Diesel cycle and greater than Otto cycle
Greater than Diesel cycle
Less than Diesel cycle
Producer gas
Coal gas
Mond gas
Coke oven gas
Plasticity
Elasticity
Ductility
Malleability
Increase in availability of energy
Increase in temperature
Decrease in pressure
Degradation of energy
The deformation of the bar per unit length in the direction of the force is called linear strain.
The Poisson's ratio is the ratio of lateral strain to the linear strain.
The ratio of change in volume to the original volume is called volumetric strain.
The bulk modulus is the ratio of linear stress to the linear strain.
Constant pressure process
Constant volume process
Constant pvn process
All of these
The liquid fuels have higher calorific value than solid fuels
The solid fuels have higher calorific value than liquid fuels
A good fuel should have low ignition point
The liquid fuels consist of hydrocarbons
Equal to
Less than
Greater than
None of these
23.97 bar
25 bar
26.03 bar
34.81 bar
Tensile in both the material
Tensile in steel and compressive in copper
Compressive in steel and tensile in copper
Compressive in both the materials
p.t.σt
d.t.σc
π/4 × d² × σt
π/4 × d² × σc
πd²/4
πd²/16
πd3/16
πd3/32
Two isothermals and two isentropic
Two isentropic and two constant volumes
Two isentropic, one constant volume and one constant pressure
Two isentropic and two constant pressures
Frequent heat treatment
Fatigue
Creep
Shock loading
Equal to
Less than
More than
None of these
δl = 4PE/ πl²
δl = 4πld²/PE
δl = 4Pl/πEd₁d₂
δl = 4PlE/ πd₁d₂
Axis of load
Perpendicular to the axis of load
Maximum moment of inertia
Minimum moment of inertia
Before point A
Beyond point A
Between points A and D
Between points D and E
Fixed at both ends
Fixed at one end and free at the other end
Supported on more than two supports
Extending beyond the supports