“…The distribution of the dimensionless circumferential strain ε(τ) = ε (2) ϕϕ (k 2 , τ) × 10 4on the outer surface ρ = k 2 is shown in Figure2a. The strain was computed from the direct problem under the thermal loading(19) for the following parameters R0 = 5.0 × 10 −2 [m], R 1 = 3.5 × 10 −2 [m], R 2 = 6.0 × 10 −2 [m], n 1 = 10 −3 [m/GPa], n 2 = 10 −4 [m/GPa], R = 5.0 × 10 −3 [m 2 × K/Wt], R * = 1.1 × 10 −3 [m 2 × K/Wt]; σ * =10 2 [MPa], T 0 = 20 [K], B = 200 [K], C = 10 2 , f = 0.25, ω = 1.22 [rad/s], and τ m = 2.5.…”