Same torque
Less torque
More torque
Unpredictable
C. More torque
wl²/3√3
wl²/6√3
wl²/9√3
wl²/12√3
K₁ K₂
(K₁ + K₂)/ 2
(K₁ + K₂)/ K₁ K₂
K₁ K₂/ (K₁ + K₂)
Plasticity
Elasticity
Ductility
Malleability
1 × 102 N/m2
1 × 103 N/m2
1 × 104 N/m2
1 × 105 N/m2
Radius
Diameter
Circumference
Area
Equal to
Less than
Greater than
None of these
Bearing stresses
Fatigue stresses
Crushing stresses
Resultant stresses
Remains constant
Increases
Decreases
None of these
Increases the internal energy of the gas
Increases the temperature of the gas
Does some external work during expansion
Both (B) and (C)
Elements
Compounds
Atoms
Molecules
Frequent heat treatment
Fatigue
Creep
Shock loading
2.1 × 10⁵ kg/cm²
2.1 × 10⁶ kg/cm²
2.1 × 10⁷ kg/cm²
0.1 × 10⁶ kg/cm²
Boyle's law
Charle's law
Gay-Lussac law
Joule's law
Resilience
Proof resilience
Strain energy
Impact energy
Top layer
Bottom layer
Neutral axis
Every cross-section
Load/original cross-sectional area and change in length/original length
Load/ instantaneous cross-sectional area and loge (original area/ instantaneous area)
Load/ instantaneous cross-sectional area and change in length/ original length
Load/ instantaneous area and instantaneous area/original area
Isothermal process
Adiabatic process
Free expansion process
Throttling process
2
4
8
16
kJ
kJ/kg
kJ/m2
kJ/m3
E = 3K.C/(3K + C)
E = 6K.C/(3K + C)
E = 9K.C/(3K + C)
E = 12K.C/(3K + C)
Loss of heat
No loss of heat
Gain of heat
No gain of heat
Brown coal
Peat
Coking bituminous coal
Non-coking bituminous coal
p.t.σt
d.t.σc
π/4 × d² × σt
π/4 × d² × σc
mR (T2 - T1)
mcv (T2 - T1)
mcp (T2 - T1)
mcp (T2 + T1)
50 %
25 %
20 %
30 %
The pressure and temperature of the working substance must not differ, appreciably, from those of the surroundings at any stage in the process
All the processes, taking place in the cycle of operation, must be extremely slow
The working parts of the engine must be friction free
All of the above
3 to 6
5 to 8
10 to 20
15 to 30
Decrease in cut-off
Increase in cut-off
Constant cut-off
None of these
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.
No heat enters or leaves the gas
The temperature of the gas changes
The change in internal energy is equal to the mechanical workdone
All of the above