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D-Index & Metrics

Mechanical and Aerospace Engineering

D-Index
46
Citations
9960
World Ranking
1415
National Ranking
557

Research.com Recognitions

  • 1998 - Fellow of the American Society of Mechanical Engineers

Overview

David G. Bogard is affiliated with The University of Texas at Austin in the United States. Their research primarily focuses on engineering, with a specialization in aerospace engineering, mechanical engineering, and computational mechanics.

The scientist's work covers several interconnected fields and topics:

  • Turbomachinery Performance and Optimization
  • Heat Transfer Mechanisms
  • Fluid Dynamics and Turbulent Flows
  • Combustion and Flame Dynamics
  • Tribology and Lubrication Engineering
  • Computational Fluid Dynamics and Aerodynamics
  • Rocket and Propulsion Systems Research

David G. Bogard has published extensively in the Journal of Turbomachinery, contributing 14 papers to this venue. Notable recent publications include:

  • Surface Curvature Effects on Film Cooling Performance for Shaped Holes on a Model Turbine Blade, 2020, Journal of Turbomachinery
  • Experimental and Computational Investigation of Integrated Internal and Film Cooling Designs Incorporating a Thermal Barrier Coating, 2022, Journal of Turbomachinery
  • Printability and Overall Cooling Performance of Additively Manufactured Holes With Inlet and Exit Rounding, 2022, Journal of Turbomachinery
  • Effects on Film Cooling Performance in the Showerhead From Geometric Parameterization of Shaped Hole Designs, 2022, Journal of Turbomachinery
  • Adiabatic Effectiveness and Thermal Field Measurements of a Shaped Hole in the Showerhead of a Model Turbine Blade, 2021, Journal of Turbomachinery

Collaboration has been an essential aspect of their research. Frequent co-authors include:

  • Michael T. Furgeson
  • Jacob D. Moore
  • Elise M. Flachs
  • Christopher Yoon
  • Karen A. Thole

David G. Bogard's research often addresses topics related to heat transfer, film cooling, and the optimization of turbine blade performance. Their work combines experimental and computational methods to investigate cooling designs and aerodynamic properties relevant to turbomachinery.

In recognition of contributions to the field, they were named a Fellow of the American Society of Mechanical Engineers in 1998.

Best Publications

  • Gas Turbine Film Cooling

    D. G. Bogard;K. A. Thole

  • Film-cooling effectiveness downstream of a single row of holes with variable density ratio

    A. K. Sinha;D. G. Bogard;M. E. Crawford

  • Film Cooling With Compound Angle Holes: Adiabatic Effectiveness

    Donald L. Schmidt;Basav Sen;David G. Bogard

  • Burst detection with single-point velocity measurements

    D. G. Bogard;W. G. Tiederman

  • Film Cooling With Compound Angle Holes: Heat Transfer

    Basav Sen;Donald L. Schmidt;David G. Bogard

  • Film Cooling With Compound Angle Holes: Adiabatic Effectiveness

    Unknown

  • Effects of Density Ratio on the Hydrodynamics of Film Cooling

    J. R. Pietrzyk;David G Bogard;M. E. Crawford

  • Hydrodynamic Measurements of Jets in Crossflow for Gas Turbine Film Cooling Applications

    J. R. Pietrzyk;David G Bogard;M. E. Crawford

  • A film-cooling correlation for shaped holes on a flat-plate surface

    Will F. Colban;Karen A. Thole;David G Bogard

  • Wall-layer structure and drag reduction

    W. G. Tiederman;T. S. Luchik;David G Bogard

  • Adiabatic Effectiveness, Thermal Fields, and Velocity Fields for Film Cooling With Large Angle Injection

    Atul Kohli;David G. Bogard

  • Comparison of RANS Turbulence Models for Prediction of Film Cooling Performance

    Katharine L. Harrison;David G. Bogard

  • Characterization and Laboratory Simulation of Turbine Airfoil Surface Roughness and Associated Heat Transfer

    David G. Bogard;Donald L. Schmidt;Martin Tabbita

  • High freestream turbulence effects on turbulent boundary layers

    K. A. Thole;David G Bogard

  • Adiabatic and Overall Effectiveness for a Film Cooled Blade

    Jason E. Albert;David G. Bogard;Frank Cunha

  • Mean temperature measurements of jets with a crossflow for gas turbine film cooling application

    K. A. Thole;A. K. Sinha;D. G. Bogard;M. E. Crawford

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

    Marcial I. Ethridge;J. Michael Cutbirth;David G. Bogard

  • High Resolution Film Cooling Effectiveness Measurements of Axial Holes Embedded in a Transverse Trench With Various Trench Configurations

    Scot K. Waye;David G. Bogard

  • Full-Coverage Film Cooling With Short Normal Injection Holes

    Mark K. Harrington;Marcus A. McWaters;David G. Bogard;Christopher A. Lemmon

  • Film Effectiveness Performance for Coolant Holes Imbedded in Various Shallow Trench and Crater Depressions

    John R. Dorrington;David G. Bogard;Ronald S. Bunker

  • Net Heat Flux Reduction and Overall Effectiveness for a Turbine Blade Leading Edge

    Brian D. Mouzon;Elon J. Terrell;Jason E. Albert;David G. Bogard

Frequent Co-Authors

Karen A. Thole
Karen A. Thole University of Michigan–Ann Arbor
Ronald Scott Bunker
Ronald Scott Bunker General Electric (United States)
Robert D. Moser
Robert D. Moser The University of Texas at Austin

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