It does not exist
It is more sensitive to changes in both metallurgical and mechanical conditions
It gives a more accurate picture of the ductility
It can be correlated with stress strain values in other tests like torsion, impact, combined stress tests etc.
A. It does not exist
Boyle's law
Charles' law
Gay-Lussac law
All of these
W1 - 2 = 0
Q1 - 2 = 0
dU = 0
All of these
Heat absorbed
Heat rejected
Either (A) or (B)
None of these
4 tonnes/ cm²
8 tonnes/ cm²
16 tonnes/ cm²
22 tonnes/ cm²
Zero
Minimum
Maximum
Positive
More
Less
Same
More/less depending on composition
Linear stress to linear strain
Linear stress to lateral strain
Volumetric strain to linear strain
Shear stress to shear strain
Not deform
Be safest
Stretch
Not stretch
Strains
Stress and strain
Shear stress and shear strain
Moduli and elasticity
Increase
Decrease
Remain unchanged
Increase/decrease depending on application
Workdone
Entropy
Enthalpy
None of these
Isothermal process
Hyperbolic process
Adiabatic process
Polytropic process
Permanent
Temporary
Semi-permanent
None of these
Butt joint
Lap joint
Double riveted lap joints
All types of joints
65° to 220°C
220° to 345°C
345° to 470°C
470° to 550°C
Principal stresses
Normal stresses on planes at 45°
Shear stresses on planes at 45°
Normal and shear stresses on a plane
(σx/2) + (1/2) × √(σx² + 4 τ²xy)
(σx/2) - (1/2) × √(σx² + 4 τ²xy)
(σx/2) + (1/2) × √(σx² - 4 τ²xy)
(1/2) × √(σx² + 4 τ²xy)
δQ = T.ds
δQ = T/ds
dQ = ds/T
None of these
-140 kJ
-80 kJ
-40 kJ
+60 kJ
Frequent heat treatment
Fatigue
Creep
Shock loading
Isothermal expansion
Isentropic expansion
Isothermal compression
Isentropic compression
12
14
16
32
wl/4
wl/2
wl
wl²/2
Thermodynamic system
Thermodynamic cycle
Thermodynamic process
Thermodynamic law
Molecular mass of the gas and the specific heat at constant volume
Atomic mass of the gas and the gas constant
Molecular mass of the gas and the gas constant
None of the above
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.
Middle of bar
Supported end
Bottom end
None of these
t
2t
4t
8t
Decrease in cut-off
Increase in cut-off
Constant cut-off
None of these
Boyle's law
Charles' law
Gay-Lussac law
Avogadro's law