Example 4.3

Description: The temperature distribution in the turbine blades exposed to hot gas flow. The turbine blades are thereby divided into equally spaced nodes, where the nods represent specific locations of the blade material. The energy equations are applied for each node taking into account the conduction effects with the neighboring nodes, and the convection effects from the surrounding gases. This allows the logical calculation to estimate the temperature distribution within the turbine blades.

Nodal temperatures for Example 4.3 (K):
T1 = 1650.15 K
T2 = 1650.82 K
T3 = 1653.52 K
T4 = 1660.44 K
T5 = 1674.78 K
T6 = 1708.13 K
T7 = 1647.49 K
T8 = 1647.83 K
T9 = 1649.55 K
T10 = 1655.15 K
T11 = 1664.27 K
T12 = 1673.80 K
T13 = 1644.16 K
T14 = 1643.47 K
T15 = 1641.69 K
T16 = 1646.35 K
T17 = 1653.34 K
T18 = 1658.54 K
T19 = 1642.19 K
T20 = 1640.22 K
T21 = 1637.60 K