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Book Title: DTIC ADA162080: Heat Transfer and Cooling in
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Book Category: TRANSIENTS
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Language: english
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Post Date: 2025-04-12 18:40:57
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PDF Size: 27.36 MB
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Book Pages: 530
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DTIC ADA162080: Heat Transfer and Cooling in
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Description of the Book:
Partial Contents: Rotating Heat Transfer on a Multipass Cooling Geometry; Pressure Drop and Heat Transfer Characteristics of Circular and Oblong Low Aspect Ratio Pin Fins; External Heat Transfer Study on a HP Turbine Rotor Blade; Effects of Wakes on the Heat Transfer in Gas Turbine Cascades; Effect of Hole Geometry, Wall Curvature and Pressure Gradient on Film Cooling Downstream of a Single Row; The Effect of Density Ratio on the Film-Cooling of a Flat Plate; Shroud Segments for Unshrouded Blade Turbines; Heat Transfer Test Evaluation of the Shell-Spar Blade Cooling Concept Applied to Industrial Gas Turbines; Heat-Flux Measurements and Analysis for a Rotating Turbine Stage; Calculation of Laminar-Turbulent Boundary Layer Transition on Turbine Blades; A Model for Correlating Flat Plate Film Cooling Effectiveness for Rows of Round Holes; Heat Transfer in Gas Turbine Combustors; Effectiveness Measurements for a Cooling Film Disrupted by a Single Jet with Wall Plunging; Full Coverage Impingement Heat Transfer: The Variation in Pitch to Diameter Ratio at a Constant Gap; The Measurement of Local Heat Transfer Coefficients in Blade Cooling Geometries; High Frequency Response Heat Flux Gauge for Metal Blading; Transient Thermal Behavior of a Compressor Rotor with Ventilation – Test Results under
Simulated Engine Conditions; Heat Exchangers in Regenerative Gas Turbine Cycles
- Creator/s: Defense Technical Information Center
- Date: 9/1/1985
- Year: 1985
- Book Topics/Themes: DTIC Archive, , ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE), *HEAT TRANSFER, *HEAT EXCHANGERS, *GAS TURBINES, *FILM COOLING, *GAS TURBINE BLADES, TEST AND EVALUATION, PRESSURE GRADIENTS, TRANSIENTS, DENSITY, MEASUREMENT, VENTILATION, COOLING, GEOMETRY, WAKE, PRESSURE, RESPONSE, HOLES(OPENINGS), CURVATURE, COMBUSTORS, REDUCTION, CYCLES, ROTOR BLADES(TURBOMACHINERY), CASCADE STRUCTURES, INDUSTRIAL EQUIPMENT, REGENERATION(ENGINEERING), HEAT TRANSFER COEFFICIENTS, FLAT PLATE MODELS, COMPRESSOR ROTORS, DOWNSTREAM FLOW, CIRCULAR, LAMINAR FLOW, HEAT FLUX, BOUNDARY LAYER TRANSITION, TRANSITIONS, EXTERNAL, WALLS, BLADES, TURBULENT FLOW, RATIOS, DIAMETERS, METALS, SIMULATION, THERMAL PROPERTIES
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