Load/original cross-sectional area and change in length/original length
Load/ instantaneous cross-sectional area and loge (original area/ instantaneous area)
Load/ instantaneous cross-sectional area and change in length/ original length
Load/ instantaneous area and instantaneous area/original area
B. Load/ instantaneous cross-sectional area and loge (original area/ instantaneous area)
Bearing stresses
Fatigue stresses
Crushing stresses
Resultant stresses
Principal stresses
Normal stresses on planes at 45°
Shear stresses on planes at 45°
Normal and shear stresses on a plane
Constant volume process
Adiabatic process
Constant pressure process
Isothermal process
Greater than
Less than
Equal to
None of these
Workdone
Entropy
Enthalpy
None of these
Inversely proportional to two times
Directly proportional to
Inversely proportional to
None of these
For a given compression ratio, both Otto and Diesel cycles have the same efficiency.
For a given compression ratio, Otto cycle is more efficient than Diesel cycle.
For a given compression ratio, Diesel cycle is more efficient than Otto cycle.
The efficiency of Otto or Diesel cycle has nothing to do with compression ratio.
log (p1p2)/log (v1v2)
log (p2/ p1)/log (v1/ v2)
log (v1/ v2)/ log (p1/p2)
log [(p1v1)/(p2v2)]
Longitudinal stress to longitudinal strain
Volumetric stress to volumetric strain
Lateral stress to Lateral strain
Shear stress to shear strain
-100 MPa
250 MPa
300 MPa
400 MPa
4/7
11/4
9/7
All of these
It is used as the alternate standard of comparison of all heat engines.
All the heat engines are based on Carnot cycle.
It provides concept of maximising work output between the two temperature limits.
All of the above
Heat
Work
Internal energy
Entropy
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
δl = 4PE/ πl²
δl = 4πld²/PE
δl = 4Pl/πEd₁d₂
δl = 4PlE/ πd₁d₂
3/7
7/3
11/3
3/11
4 tonnes/ cm²
8 tonnes/ cm²
16 tonnes/ cm²
22 tonnes/ cm²
Petrol engine
Diesel engine
Reversible engine
Irreversible engine
Low
Very low
High
Very high
Same
Lower
Higher
None of these
Isothermal process
Hyperbolic process
Adiabatic process
Polytropic process
External energy
Internal energy
Kinetic energy
Molecular energy
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
It is impossible to construct an engine working on a cyclic process, whose sole purpose is to convert heat energy into work
It is possible to construct an engine working on a cyclic process, whose sole purpose is to convert heat energy into work
It is impossible to construct a device which operates in a cyclic process and produces no effect other than the transfer of heat from a cold body to a hot body
None of the above
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 force changes sign
Bending moment changes sign
Shear force is maximum
Bending moment is maximum
Frequent heat treatment
Fatigue
Creep
Shock loading
Isothermally
Isentropically
Polytropically
None of these
Rankine
Stirling
Carnot
Brayton
Carnot
Ericsson
Stirling
None of the above