A. Bölcs

Actuators for Active Flow Control

Evaluation of Pressure Side Film Cooling With Flow and Thermal Field Measurements—Part I: Showerhead Effects

An experimental investigation of boundary layer ingestion in a diffusing S-duct with and without passive flow control

Review of research on low-profile vortex generators to control boundary-layer separation

Heat Flux Reduction From Film Cooling and Correlation of Heat Transfer Coefficients From Thermographic Measurements at Enginelike Conditions

Thermal Field and Flow Visualization Within the Stagnation Region of a Film-Cooled Turbine Vane

A Review of Shaped Hole Turbine Film-Cooling Technology

Free-Stream Turbulence Effects on Film Cooling With Shaped Holes

Assessment of Various Film-Cooling Configurations Including Shaped and Compound Angle Holes Based on Large-Scale Experiments

Use of High-Speed Microjets for Active Separation Control in Diffusers

Correlation of Film-Cooling Effectiveness From Thermographic Measurements at Enginelike Conditions

Scaling of Performance for Varying Density Ratio Coolants on an Airfoil With Strong Curvature and Pressure Gradient Effects

Gas Turbine Film Cooling

Design of the Blended Wing Body Subsonic Transport

Scaling of Performance for Varying Density Ratio Coolants on an Airfoil With Strong Curvature and Pressure Gradient Effects

Experimental Study of Showerhead Cooling on a Cylinder Comparing Several Configurations Using Cylindrical and Shaped Holes

Experimental Study of Showerhead Cooling on a Cylinder Comparing Several Configurations Using Cylindrical and Shaped Holes

Performance of a Turbine Airfoil with Multiple Film Cooling Stations - Part I : Heat Transfer and Film Cooling Effectiveness

Influence of inlet distortion on transonic compressor blade loading

Performance of a Turbine Airfoil With Multiple Film Cooling Stations: Part II — Aerodynamic Losses

An Investigation of Effectiveness and Heat Transfer on a Showerhead-Cooled Cylinder

Utilization of the Transient Liquid Crystal Technique for Film Cooling Effectiveness and Heat Transfer Investigations on a Flat Plate and a Turbine Airfoil