Defence Science Journal
  • Year: 2007
  • Volume: 57
  • Issue: 2

Creep transition in a thin rotating disc with rigid inclusion

  • Author:
  • S.K. Gupta, Pankaj
  • Total Page Count: 11
  • Page Number: 185 to 195

H.P. University, Shimla-171 005.

Abstract

Creep stresses and strain rates have been obtained for a thin rotating disc with inclusion using Seth's transition theory. Results have been discussed numerically and depicted graphically. It has been observed that radial stress has maximum value at the internal surface of the rotating disc made of incompressible material as compared to circumferential stress and this value of radial stress further increases with the increase in angular speed. Strain rates have maximum values at the internal surface for compressible material. Rotating disc is likely to fracture by cleavage close to the inclusion at the bore

A

Principal finite strain components

eii

Internal and external radii of the disc

u,v,w

Displacement components

r,θ,z

Radial, circumferential and axial directions

ω

Angular velocity of rotation

δ

Kronecker's delta

ρ

Density of material

C

Compressibility factor

ėtj

Strain rate tensor

Y

Yield stress

εij

Swainger strain components

v

Poisson's ratio

2

ρω2b2/E (Speed factor); R=r/b; R0=a/b

σr

Radial stress component (Trr/E)

σθ

Circumferential stress component (Tθθ/E)

Keywords

Creep stress, thin rotating disc, stress, strain, rotors, turbines, creep transition, solid mechanics