Accession Number:

ADA162080

Title:

Heat Transfer and Cooling in Gas Turbines

Descriptive Note:

Conference proceedings

Corporate Author:

ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE)

Personal Author(s):

Report Date:

1985-09-01

Pagination or Media Count:

530.0

Abstract:

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.

Subject Categories:

  • Thermodynamics
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE