Change the shape of the beam
Effect the saving in material
Equalise the strength in tension and compression
Increase the cross-section of the beam
C. Equalise the strength in tension and compression
Hookes law
Yield point
Plastic flow
Proof stress
Butt joint
Lap joint
Double riveted lap joints
All types of joints
Always in single shear
Always in double shear
Either in single shear or double shear
None of these
Carnot cycle
Rankine cycle
Brayton cycle
Bell Coleman cycle
One-half
One-third
Two-third
Three-fourth
Straight line formula
Eulers formula
Rankines formula
Secant formula
It is impossible to construct an engine working on a cyclic process, whose sole purpose is to convert heat energy into work.
It is impossible to transfer heat from a body at a lower temperature to a higher temperature, without the aid of an external source.
There is a definite amount of mechanical energy, which can be obtained from a given quantity of heat energy.
All of the above
Isothermal process
Adiabatic process
Hyperbolic process
Polytropic process
In the middle
At the tip below the load
At the support
Anywhere
Heat
Work
Internal energy
Entropy
Linear stress to linear strain
Linear stress to lateral strain
Volumetric strain to linear strain
Shear stress to shear strain
5WL³/ 384EI
WL³/384EI
WL³/ 348EI
WL³/ 48EI
rγ - 1
1 - rγ - 1
1 - (1/r) γ/γ - 1
1 - (1/r) γ - 1/ γ
A Joule cycle consists of two constant volume and two isentropic processes.
An Otto cycle consists of two constant volume and two isentropic processes.
An Ericsson cycle consists of two constant pressure and two isothermal processes.
All of the above
3 to 6
5 to 8
15 to 20
20 to 30
p v = constant, if T is kept constant
v/T = constant, if p is kept constant
p/T = constant, if v is kept constant
T/p = constant, if v is kept constant
Constant volume
Constant temperature
Constant pressure
None of these
1 kg of water
7 kg of water
8 kg of water
9 kg of water
0.287 J/kgK
2.87 J/kgK
28.7 J/kgK
287 J/kgK
The axis of load
An oblique plane
At right angles to the axis of specimen
Would not occur
Its own length
Twice its length
Half its length
1/√2 × its length
1.817
2512
4.187
None of these
Bearing stresses
Fatigue stresses
Crushing stresses
Resultant stresses
Absolute pressure = Gauge pressure + Atmospheric pressure
Gauge pressure = Absolute pressure + Atmospheric pressure
Atmospheric pressure = Absolute pressure + Gauge pressure
Absolute pressure = Gauge pressure - Atmospheric pressure
(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
Q1 - 2 = dU + W1 - 2
Q1 - 2 = dU - W1 - 2
Q1 - 2 = dU/W1 - 2
Q1 - 2 = dU × W1 - 2
t
2t
4t
8t
Equal to one
Less than one
Greater than one
None of these
(p2/p1)γ - 1/ γ
(p1/p2)γ - 1/ γ
(v2/v1)γ - 1/ γ
(v1/v2)γ - 1/ γ
Isothermal
Isentropic
Polytropic
None of these