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RISDiscussion: “Gas Turbine Blade Heat Transfer Augmentation by Impingement of Air Jets Having Various Configurations” (Tabakoff, W., and Clevenger, W., 1972, ASME J. Eng. Power, 94, pp. 51–58)
Publisher: The American Society of Mechanical Engineers (ASME)
Discussion: “Effects of Crossflow on Impingement Heat Transfer” (Metzger, D. E., and Korstad, R. J., 1972, ASME J. Eng. Power, 94, pp. 35–41)
Publisher: The American Society of Mechanical Engineers (ASME)
Time-Averaged Heat-Flux Distributions and Comparison With Prediction for the Teledyne 702 HP Turbine Stage
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Time-averaged heat-flux distributions are reported for the vane and blade of the Teledyne CAE 702 HP full-stage rotating turbine. A shock tube is used as a short-duration source of heated air ...
Generalizing Circular Brush Seal Leakage Through a Randomly Distributed Bristle Bed
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Brush seals have established a niche in the gas-to-gas sealing against leakage in modern turbine engines. The variable nature of the brush during operation makes leakage prediction difficult. A ...
Performance Characteristics of Brush Seals for Limited-Life Engines
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Brush seals are potential replacements for air-to-air labyrinth seals in gas turbine engines. An investigation has been conducted to determine the performance characteristics of brush seals for ...
Phase-Resolved Heat-Flux Measurements on the Blade of a Full-Scale Rotating Turbine
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper presents detailed phase-resolved heat-flux data obtained on the blade of a Teledyne 702 HP full-stage rotating turbine. A shock tube is used as a short-duration source of heated air ...