Linear stress to linear strain
Linear stress to lateral strain
Volumetric strain to linear strain
Shear stress to shear strain
D. Shear stress to shear strain
Zero
Minimum
Maximum
Infinity
√(KT/m)
√(2KT/m)
√(3KT/m)
√(5KT/m)
Isothermally
Isentropically
Polytropically
None of these
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
Same
More
Less
Unpredictable
Slenderness ratio and area of cross-section
Poisson's ratio and modulus of elasticity
Slenderness ratio and modulus of elasticity
Slenderness ratio, area of cross-section and modulus of elasticity
Boyle's law
Charles' law
Gay-Lussac law
Avogadro's law
Conservation of work
Conservation of heat
Conversion of heat into work
Conversion of work into heat
Greater than
Less than
Equal to
None of these
δl = 4PE/ πl²
δl = 4πld²/PE
δl = 4Pl/πEd₁d₂
δl = 4PlE/ πd₁d₂
There is no change in temperature
There is no change in enthalpy
There is no change in internal energy
All of these
Lap joint
Butt joint
Single riveted single cover butt joint
Double riveted double cover butt joint
Pressure exerted by the gas
Volume occupied by the gas
Temperature of the gas
All of these
Cracking
Carbonisation
Fractional distillation
Full distillation
Increase
Decrease
Remain unchanged
Increase/decrease depending on application
Coke
Wood charcoal
Bituminous coal
Briquetted coal
Malleability
Ductility
Plasticity
Elasticity
Pressure and temperature
Temperature and volume
Heat and work
All of these
Linear stress to lateral strain
Lateral strain to linear strain
Linear stress to linear strain
Shear stress to shear strain
Producer gas
Coal gas
Mond gas
Coke oven gas
Same
Double
Half
Four times
Molecular mass of the gas and the gas constant
Atomic mass of the gas and the gas constant
Molecular mass of the gas and the specific heat at constant pressure
Molecular mass of the gas and the specific heat at constant volume
Bending moment (i.e. M)
Bending moment² (i.e. M²)
Bending moment³ (i.e. M³)
Bending moment⁴ (i.e. M⁴)
0
1
γ
∝
2
8
16
32
12
14
16
32
Principal stresses
Normal stresses on planes at 45°
Shear stresses on planes at 45°
Normal and shear stresses on a plane
Working substance
Design of engine
Size of engine
Temperatures of source and sink
Equal to
Half
Double
Quadruple
Reversible
Irreversible
Reversible or irreversible
None of these