Remains constant
Decreases
Increases
None of these
C. Increases
(Net work output)/(Workdone by the turbine)
(Net work output)/(Heat supplied)
(Actual temperature drop)/(Isentropic temperature drop)
(Isentropic increase in temperature)/(Actual increase in temperature)
Plastic limit
Elastic limit
Yield point
Limit of proportionality
d/4
d/8
d/12
d/16
Middle of bar
Supported end
Bottom end
None of these
2.1 × 10⁵ kg/cm²
2.1 × 10⁶ kg/cm²
2.1 × 10⁷ kg/cm²
0.1 × 10⁶ kg/cm²
Hookes law
Yield point
Plastic flow
Proof stress
3 to 6
5 to 8
10 to 20
15 to 30
Axis of load
Perpendicular to the axis of load
Maximum moment of inertia
Minimum moment of inertia
1.333 N/m2
13.33 N/m2
133.3 N/m2
1333 N/m2
Fixed at both ends
Fixed at one end and free at the other end
Supported at its ends
Supported on more than two supports
0.4 radian
0.8 radian
1.6 radian
3.2 radian
δl = 4PE/ πl²
δl = 4πld²/PE
δl = 4Pl/πEd₁d₂
δl = 4PlE/ πd₁d₂
Maximum cycle temperature
Minimum cycle temperature
Pressure ratio
All of these
12
14
16
32
For a given compression ratio, both Otto and Diesel cycles have the same efficiency.
For a given compression ratio, Otto cycle is more efficient than Diesel cycle.
For a given compression ratio, Diesel cycle is more efficient than Otto cycle.
The efficiency of Otto or Diesel cycle has nothing to do with compression ratio.
δQ = T.ds
δQ = T/ds
dQ = ds/T
None of these
Swept volume to total volume
Total volume to swept volume
Swept volume to clearance volume
Total volume to clearance volume
Increase in availability of energy
Increase in temperature
Decrease in pressure
Degradation of energy
Zeroth law of thermodynamics
First law of thermodynamics
Second law of thermodynamics
Kinetic theory of gases
Wood charcoal
Bituminous coke
Pulverised coal
Coke
Tensile strain increases more quickly
Tensile strain decreases more quickly
Tensile strain increases in proportion to the stress
Tensile strain decreases in proportion to the stress
One-half
One-third
Two-third
Three-fourth
Isothermal process
Hyperbolic process
Adiabatic process
Polytropic process
Rubber
Plastic
Brass
Steel
-273°C
73°C
237°C
-237°C
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.
From maximum at the centre to zero at the circumference
From zero at the centre to maximum at the circumference
From maximum at the centre to minimum at the circumference
From minimum at the centre to maximum at the circumference
Tensile stress
Compressive stress
Shear stress
Strain
Absolute scale of temperature
Absolute zero temperature
Absolute temperature
None of these
Oxygen
Sulphur
Nitrogen
Carbon