Problems of Heat Transfer in Gas Turbines (Collection of Articles)
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH
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The articles in this collection contain the results of theoretical and experimental studies of heat transfer in gas turbines, and the temperature states of turbine blades, disks, and rotors. Analysis is given of the boundary conditions formulated when stating problems of thermal conductivity relative to gas turbines. Results are given of a generalization of criterial formulas for calculating the heat-transfer coefficient in vane cascades. Certain specific problems of thermal conductivity are solved in general form and numerically for cooled hollow blades and disks.
- Jet and Gas Turbine Engines