Tensile stress
Compressive stress
Shear stress
Thermal stress
D. Thermal stress
1 × 102 N/m2
1 × 103 N/m2
1 × 104 N/m2
1 × 105 N/m2
Mass of oxygen in 1 kg of flue gas to the mass of oxygen in 1 kg of fuel
Mass of oxygen in 1 kg of fuel to the mass of oxygen in 1 kg of flue gas
Mass of carbon in 1 kg of flue gas to the mass of carbon in 1 kg of fuel
Mass of carbon in 1 kg of fuel to the mass of carbon in 1 kg of flue gas
Plasticity
Elasticity
Ductility
Malleability
Temperature limits
Pressure ratio
Compression ratio
Cut-off ratio and compression ratio
Its temperature will increase
Its pressure will increase
Both temperature and pressure will increase
Neither temperature nor pressure will increase
300° to 500°C
500° to 700°C
700° to 900°C
900° to 1100°C
Vapour
Perfect gas
Air
Steam
Otto cycle is more efficient than Diesel cycle
Diesel cycle is more efficient than Otto cycle
Dual cycle is more efficient than Otto and Diesel cycles
Dual cycle is less efficient than Otto and Diesel cycles
Energy stored in a body when strained within elastic limits
Energy stored in a body when strained up to the breaking of a specimen
Maximum strain energy which can be stored in a body
Proof resilience per unit volume of a material
Pressure
Volume
Temperature
All of these
Carnot cycle
Rankine cycle
Brayton cycle
Bell Coleman cycle
In tension
In compression
Neither in tension nor in compression
None of these
The shaft 'B' has the greater diameter
The shaft 'A' has the greater diameter
Both are of same diameter
None of these
Same
Lower
Higher
None of these
Partial combustion of coal, coke, anthracite coal or charcoal in a mixed air steam blast
Carbonisation of bituminous coal
Passing steam over incandescent coke
Passing air and a large amount of steam over waste coal at about 650°C
External energy
Internal energy
Kinetic energy
Molecular energy
Sum
Difference
Multiplication
None of the above
Constant pressure process
Constant volume process
Constant pvn process
All of these
(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]
Equal to
Directly proportional to
Inversely proportional to
None of these
It is possible to transfer heat from a body at a lower temperature to a body at a higher temperature.
It is impossible to transfer heat from a body at a lower temperature to a body at a higher temperature, without the aid of an external source.
It is possible to transfer heat from a body at a lower temperature to a body at a higher temperature by using refrigeration cycle.
None of the above
Oxygen
Sulphur
Nitrogen
Carbon
Thermodynamic system
Thermodynamic cycle
Thermodynamic process
Thermodynamic law
e (1 - 2m)
e (1 - 2/m)
e (m - 2)
e (2/m - 1)
Constant pressure cycle
Constant volume cycle
Constant temperature cycle
Constant temperature and pressure cycle
Heat transfer is constant
Work transfer is constant
Mass flow at inlet and outlet is same
All of these
2ε₁ - ε₂
2ε₁ + ε₂
2ε₂ - ε₁
2ε₂ + ε₁
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.
Working substance
Design of engine
Size of engine
Temperatures of source and sink
0
1
γ
∝