Acts at a point on a beam
Spreads non-uniformly over the whole length of a beam
Spreads uniformly over the whole length of a beam
Varies uniformly over the whole length of a beam
A. Acts at a point on a beam
Rankine
Stirling
Carnot
Brayton
Perfect gas
Air
Steam
Ordinary gas
Zero
wl/4
wl/2
wl²/2
The stress is the pressure per unit area
The strain is expressed in mm
Hook's law holds good upto the breaking point
Stress is directly proportional to strain within elastic limit
π /4 × τ × D³
π /16 × τ × D³
π /32 × τ × D³
π /64 × τ × D³
(p1 v1 - p2 v2)/(γ - 1)
[m R (T1 - T2)] /(γ - 1)
[m R T1/(γ - 1)][1 - (p2 v2 /p1 v1)]
All of these
Elastic point of the material
Plastic point of the material
Breaking point of the material
Yielding point of the material
There is no change in temperature
There is no change in enthalpy
There is no change in internal energy
All of these
Pressure and temperature
Temperature and volume
Heat and work
All of these
The deformation of the bar per unit length in the direction of the force is called linear strain.
The Poisson's ratio is the ratio of lateral strain to the linear strain.
The ratio of change in volume to the original volume is called volumetric strain.
The bulk modulus is the ratio of linear stress to the linear strain.
The amount of heat required to raise the temperature of unit mass of gas through one degree, at constant pressure
The amount of heat required to raise the temperature of unit mass of gas through one degree, at constant volume
The amount of heat required to raise the temperature of 1 kg of water through one degree
Any one of the above
Constant volume process
Adiabatic process
Constant pressure process
Isothermal process
Heat transfer is constant
Work transfer is constant
Mass flow at inlet and outlet is same
All of these
Maximum torque it can transmit
Number of cycles it undergoes before failure
Elastic limit up to which it resists torsion, shear and bending stresses
Torque required to produce a twist of one radian per unit length of shaft
Th > Ts
Th < Ts
Th = Ts
None of these
Becomes constant
Starts decreasing
Increases without any increase in load
None of the above
Greater than
Less than
Equal to
None of these
Increase in availability of energy
Increase in temperature
Decrease in pressure
Degradation of energy
Increase
Decrease
Remain unchanged
Increase/decrease depending on application
Of same magnitude as that of bar and applied at the lower end
Half the weight of bar applied at lower end
Half of the square of weight of bar applied at lower end
One fourth of weight of bar applied at lower end
Ultimate shear stress of the column
Factor of safety
Torque resisting capacity
Slenderness ratio
0.5 s.l.σt
s.l.σt
√2 s.l.σt
2.s.l.σt
Frequent heat treatment
Fatigue
Creep
Shock loading
(23/100) × Mass of excess carbon
(23/100) × Mass of excess oxygen
(100/23) × Mass of excess carbon
(100/23) × Mass of excess oxygen
Swept volume to total volume
Total volume to swept volume
Swept volume to clearance volume
Total volume to clearance volume
Increases power output
Improves thermal efficiency
Reduces exhaust temperature
Do not damage turbine blades
Tensile strain increases more quickly
Tensile strain decreases more quickly
Tensile strain increases in proportion to the stress
Tensile strain decreases in proportion to the stress
Shear modulus
Section modulus
Polar modulus
None of these
0
1
γ
∝
Boyle's law
Charles' law
Gay-Lussac law
Joule's law