Zero
1/5
4/5
1
A. Zero
Boyle's law
Charles' law
Gay-Lussac law
Avogadro's law
Two constant pressure
Two constant volume
Two isentropic
One constant pressure, one constant volume
1
0
-1
10
Carnot
Stirling
Ericsson
None of the above
pv = mRT
pv = RTm
pvm = C
pv = (RT)m
Straight line formula
Eulers formula
Rankines formula
Secant formula
Strain energy
Resilience
Proof resilience
Modulus of resilience
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
The heat and work are boundary phenomena
The heat and work represent the energy crossing the boundary of the system
The heat and work are path functions
All of the above
3 to 6
5 to 8
15 to 20
20 to 30
Two constant volume and two isentropic processes
Two constant volume and two isothermal processes
Two constant pressure and two isothermal processes
One constant volume, one constant pressure and two isentropic processes
Coal gas
Producer gas
Mond gas
Blast furnace gas
√(KT/m)
√(2KT/m)
√(3KT/m)
√(5KT/m)
Boyle's law
Charle's law
Gay-Lussac law
Joule's law
kJ
kJ/kg
kJ/m2
kJ/m3
Joint less section
Homogeneous section
Perfect section
Seamless section
2ε₁ - ε₂
2ε₁ + ε₂
2ε₂ - ε₁
2ε₂ + ε₁
Otto cycle is more efficient than Diesel cycle
Diesel cycle is more efficient than Otto cycle
Efficiency depends on other factors
Both Otto and Diesel cycles are equally efficient
Carnot cycle
Bell-Coleman cycle
Rankine cycle
Stirling cycle
Boyle's law
Charles' law
Gay-Lussac law
Joule's law
0.01 to 0.1
0.23 to 0.27
0.25 to 0.33
0.4 to 0.6
Pressure exerted by the gas
Volume occupied by the gas
Temperature of the gas
All of these
Mechanical and fluid friction
Unrestricted expansion
Heat transfer with a finite temperature difference
All of the above
Mono-atomic
Di-atomic
Tri-atomic
Poly-atomic
Reversible process
Irreversible process
Reversible or irreversible process
None of these
Bearing stresses
Fatigue stresses
Crushing stresses
Resultant stresses
1 - rγ - 1
1 + rγ - 1
1 - (1/ rγ - 1)
1 + (1/ rγ - 1)
Absolute pressure = Gauge pressure + Atmospheric pressure
Gauge pressure = Absolute pressure + Atmospheric pressure
Atmospheric pressure = Absolute pressure + Gauge pressure
Absolute pressure = Gauge pressure - Atmospheric pressure
Yield point stress
Breaking stress
Ultimate stress
Elastic limit
Element
Compound
Atom
Molecule