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
D. Two isentropic and two constant pressures
1 × 102 N/m2
1 × 103 N/m2
1 × 104 N/m2
1 × 105 N/m2
Sum of two principal stresses
Difference of two principal stresses
Half the sum of two principal stresses
Half the difference of two principal stresses
No stress
Shear stress
Tensile stress
Compressive stress
Young's modulus
Bulk modulus
Modulus of rigidity
Modulus of elasticity
Same as
Less than
Greater than
None of these
log (p1p2)/log (v1v2)
log (p2/ p1)/log (v1/ v2)
log (v1/ v2)/ log (p1/p2)
log [(p1v1)/(p2v2)]
First kind
Second kind
Third kind
None of these
Equal to
Less than
More than
None of these
In the vertical plane
In the horizontal plane
In the same plane in which the beam bends
At right angle to the plane in which the beam bends
Zeroth law of thermodynamics
First law of thermodynamics
Second law of thermodynamics
Kinetic theory of gases
When molecular momentum of the system becomes zero
At sea level
At the temperature of - 273 K
At the centre of the earth
400 MPa
500 MPa
900 MPa
1400 MPa
Not deform
Be safest
Stretch
Not stretch
1 - rγ - 1
1 + rγ - 1
1 - (1/ rγ - 1)
1 + (1/ rγ - 1)
Proportional limit, elastic limit, yielding, failure
Elastic limit, proportional limit, yielding, failure
Yielding, proportional limit, elastic limit, failure
None of the above
Considerably greater than that necessary to continue it
Considerably lesser than that necessary to continue it
Greater than that necessary to stop it
Lesser than that necessary to stop it
Pressure exerted by the gas
Volume occupied by the gas
Temperature of the gas
All of these
Always in single shear
Always in double shear
Either in single shear or double shear
None of these
Bending moment (i.e. M)
Bending moment² (i.e. M²)
Bending moment³ (i.e. M³)
Bending moment⁴ (i.e. M⁴)
WD3n/Cd⁴
2WD3n/Cd⁴
4WD3n/Cd⁴
8WD3n/Cd⁴
Zeroth law of thermodynamics
First law of thermodynamics
Second law of thermodynamics
None of these
In tension
In compression
Neither in tension nor in compression
None of these
Same torque
Less torque
More torque
Unpredictable
Zero
Minimum
Maximum
Infinity
The closed cycle gas turbine plants are external combustion plants.
In the closed cycle gas turbine, the pressure range depends upon the atmospheric pressure.
The advantage of efficient internal combustion is eliminated as the closed cycle has an external surface.
In open cycle gas turbine, atmosphere acts as a sink and no coolant is required.
50 %
25 %
20 %
30 %
5WL³/ 384EI
WL³/384EI
WL³/ 348EI
WL³/ 48EI
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
cv/ cp =R
cp - cv = R
cv = R/ γ-1
Both (B) and (C)
It is used as the alternate standard of comparison of all heat engines.
All the heat engines are based on Carnot cycle.
It provides concept of maximising work output between the two temperature limits.
All of the above