Increases power output
Improves thermal efficiency
Reduces exhaust temperature
Do not damage turbine blades
C. Reduces exhaust temperature
Straight line formula
Eulers formula
Rankines formula
Secant formula
Increases power output
Improves thermal efficiency
Reduces exhaust temperature
Do not damage turbine blades
τ²/ 2G × Volume of shaft
τ/ 2G × Volume of shaft
τ²/ 4G × Volume of shaft
τ/ 4G × Volume of shaft
1.817
2512
4.187
None of these
Maximum shear stress
No shear stress
Minimum shear stress
None of the above
Frequent heat treatment
Fatigue
Creep
Shock loading
Thermal efficiency
Work ratio
Avoids pollution
None of these
23.97 bar
25 bar
26.03 bar
34.81 bar
0
1
γ
∝
Calorific value
Heat energy
Lower calorific value
Higher calorific value
Petrol engine
Diesel engine
Reversible engine
Irreversible engine
Constant volume process
Adiabatic process
Constant pressure process
Isothermal process
(σx + σy)/2 + (1/2) × √[(σx - σy)² + 4 τ²xy]
(σx + σy)/2 - (1/2) × √[(σx - σy)² + 4 τ²xy]
(σx - σy)/2 + (1/2) × √[(σx + σy)² + 4 τ²xy]
(σx - σy)/2 - (1/2) × √[(σx + σy)² + 4 τ²xy]
Sum
Difference
Multiplication
None of the above
Very low
Low
High
Very high
Greater than
Less than
Equal to
None of these
Increase
Decrease
Remain unchanged
Increase/decrease depending on application
When coal is first dried and then crushed to a fine powder by pulverising machine
From the finely ground coal by moulding under pressure with or without a binding material
When coal is strongly heated continuously for 42 to 48 hours in the absence of air in a closed vessel
By heating wood with a limited supply of air to a temperature not less than 280°C
300° to 500°C
500° to 700°C
700° to 900°C
900° to 1100°C
Linear stress to lateral strain
Lateral strain to linear strain
Linear stress to linear strain
Shear stress to shear strain
When molecular momentum of the system becomes zero
At sea level
At the temperature of - 273 K
At the centre of the earth
Young's modulus
Bulk modulus
Modulus of rigidity
Poisson's ratio
Rankine
Stirling
Carnot
Brayton
Principal stresses
Normal stresses on planes at 45°
Shear stresses on planes at 45°
Normal and shear stresses on a plane
Carnot
Stirling
Ericsson
None of the above
1.333 N/m2
13.33 N/m2
133.3 N/m2
1333 N/m2
W1 - 2 = 0
Q1 - 2 = 0
dU = 0
All of these
Proportional limit, elastic limit, yielding, failure
Elastic limit, proportional limit, yielding, failure
Yielding, proportional limit, elastic limit, failure
None of the above
Carnot cycle can't work with saturated steam
Heat is supplied to water at temperature below the maximum temperature of the cycle
A Rankine cycle receives heat at two places
Rankine cycle is hypothetical
(23/100) × Mass of excess carbon
(23/100) × Mass of excess oxygen
(100/23) × Mass of excess carbon
(100/23) × Mass of excess oxygen