Faculty

Institution

Unit

Venue

David Bogard

Professor

University of Texas at Austin

Affiliations

Cockrell School of Engineering

Walker Department of Mechanical Engineering

David Bogard is currently serving as a Cockrell School Of Engineering Professor at University of Texas At Austin.

Honors

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Experiences

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Education

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David Bogard

University of Texas at Austin

Professor

You can click a keyword to filter the displayed items

thermal engineering mechanical engineering heat transfer engineering turbomachinery applied physics aerospace engineering fluid dynamics aerodynamics turbine vane fluid mechanics performance evaluation film cooling overall effectiveness adiabatic effectiveness suction side experimental analysis thermal barrier coatings shaped holes gas turbine vane materials engineering numerical simulations turbulence modeling gas turbine engines turbine blade surface roughness surface science additive manufacturing engineering optimization engineering thermodynamics hydraulics boundary layers heat mass transfer aeronautics aerospace technology thermal management gas turbine combustion fluid machinery compound angle holes transverse trench experimental simulation cfd predictions adiabatic effectiveness values experimental measurements simulated turbine vane propulsion advanced manufacturing technologies fluid flow metals benchmark studies thermal processing turbulent flow heat transfer convective heat transfer compressor computational fluid dynamics sustainable energy technologies power electronics manufacturing technology hydraulic engineering ventilation continual improvement process dispersion comparative analysis oscillation theory thermal energy energy engineering aerial robotics astronautics precision measurement unsteady flows thermal analysis structure determination feedback loop

Notable Scholarly Works

Notable Federal Grants

Collaborators

Adjoint Optimization of Gas Turbine Film Cooling Geometry With Elevated Mainstream Mach Number. (2025)

numerical simulationsgas turbine enginescomputational engineeringengineeringmechanical engineeringthermal managementnumerical analysisaerospace engineering

Design and Fabrication of a Thermally Optimized Gas Turbine Nozzle. Journal of Turbomachinery (2025)

energy transformationgas turbine enginesengineeringhydraulic machineryheat transfergas turbine combustionfluid machinerymechanical engineeringthermal engineeringcompressorheat mass transferturbomachinery

Elevated Mainstream Mach Number Effects on Shaped Gas Turbine Film Cooling Holes. Journal of Turbomachinery (2025)

gas turbine enginesengineeringgas turbine combustionaerodynamicsfluid machineryfluid dynamicsmechanical engineeringaerospace engineeringturbomachinery

Investigation Into the Optimal Gas Turbine Film Cooling Configuration With the Use of a Thermal Barrier Coating. (2025)

energy conversiongas turbine enginesengineeringthermal barrier coatingsheat transfercoatingsenergy efficiencythermal engineeringthermal protection

Performance and Evaluation of a Thermally Optimized Gas Turbine Nozzle. Journal of Turbomachinery (2025)

energy transformationgas turbine enginesengineeringheat transfergas turbine combustionfluid machinerymechanical engineeringthermal engineeringcompressorheat mass transferturbomachinery

Considerations for Compressible Film Cooling: A Computational Study of the Effects of Transonic Flows and Varying Mainstream Mach Number. Journal of Turbomachinery (2024)

Dale W. FoxMichael FurgesonDavid G. Bogard

mainstream mach numbercomputational studyengineeringheat transfermechanical engineeringcompressible film coolingtransonic flowsthermal engineeringapplied physicsturbomachinery

Evaluations of Superposition Predictions of Adiabatic and Overall Effectiveness for Three Rows of Film Cooling Holes With Differing Hole Geometries. (2024)

Molly E. EllingerElise M. FlachsAmeya N. KulkarniDavid G. Bogard

numerical simulationsmetalsmechanical engineeringapplied physicsoptical propertiesfeedback loopperformance evaluationheat transfertheoretical predictionoverall effectivenesselectrical engineeringsuperposition predictionsthermal engineeringsource apportionmentthin filmssorption coolingsurface sciencehole geometriescryogenics

Integrated Turbine Component Cooling Designs Facilitated by Additive Manufacturing and Optimization. (2024)

David BogardTodd OliverKaren Thole

design optimizationengineeringheat transfermechanical engineeringthermal engineeringadditive manufacturingmanufacturingengineering optimization

Investigation of the Effects of Geometry Variations on the Performance of an Adjoint Optimized Film Cooling Hole. Heat Transfer (2024)

Molly E. EllingerElise M. FlachsDavid G. Bogard

numerical simulationsmetalsfilmmesh optimizationmechanical engineeringenergy conversionperformance evaluationheat transfergeometry processingheat mass transfergeometry variationsenvironmental engineeringcoatingsthermal engineeringthin filmsconvective heat transferdesign optimizationthin film processingthermal conduction

Overall Cooling Effectiveness With Internal Serpentine Channels and Optimized Film Cooling Holes. Journal of Turbomachinery (2024)

Christopher YoonElise M. FlachsMolly E. EllingerDavid G. Bogard

internal serpentine channelsengineeringheat transfermechanical engineeringthermal engineeringturbomachinery

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David Bogard

Professor

University of Texas at Austin

Affiliations

Cockrell School of Engineering

Walker Department of Mechanical Engineering

David Bogard is currently serving as a Cockrell School Of Engineering Professor at University of Texas At Austin.

Honors

Create free account to unlock more features

Experiences

Create free account to unlock more features

Education

Create free account to unlock more features

David Bogard

University of Texas at Austin

Professor

You can click a keyword to filter the displayed items

Notable Scholarly Works

Notable Federal Grants

Collaborators

Adjoint Optimization of Gas Turbine Film Cooling Geometry With Elevated Mainstream Mach Number. (2025)

numerical simulationsgas turbine enginescomputational engineeringengineeringmechanical engineeringthermal managementnumerical analysisaerospace engineering

Design and Fabrication of a Thermally Optimized Gas Turbine Nozzle. Journal of Turbomachinery (2025)

Elevated Mainstream Mach Number Effects on Shaped Gas Turbine Film Cooling Holes. Journal of Turbomachinery (2025)

gas turbine enginesengineeringgas turbine combustionaerodynamicsfluid machineryfluid dynamicsmechanical engineeringaerospace engineeringturbomachinery

Investigation Into the Optimal Gas Turbine Film Cooling Configuration With the Use of a Thermal Barrier Coating. (2025)

energy conversiongas turbine enginesengineeringthermal barrier coatingsheat transfercoatingsenergy efficiencythermal engineeringthermal protection

Performance and Evaluation of a Thermally Optimized Gas Turbine Nozzle. Journal of Turbomachinery (2025)

energy transformationgas turbine enginesengineeringheat transfergas turbine combustionfluid machinerymechanical engineeringthermal engineeringcompressorheat mass transferturbomachinery

Considerations for Compressible Film Cooling: A Computational Study of the Effects of Transonic Flows and Varying Mainstream Mach Number. Journal of Turbomachinery (2024)

Dale W. FoxMichael FurgesonDavid G. Bogard

mainstream mach numbercomputational studyengineeringheat transfermechanical engineeringcompressible film coolingtransonic flowsthermal engineeringapplied physicsturbomachinery

Evaluations of Superposition Predictions of Adiabatic and Overall Effectiveness for Three Rows of Film Cooling Holes With Differing Hole Geometries. (2024)

Molly E. EllingerElise M. FlachsAmeya N. KulkarniDavid G. Bogard

Integrated Turbine Component Cooling Designs Facilitated by Additive Manufacturing and Optimization. (2024)

David BogardTodd OliverKaren Thole

design optimizationengineeringheat transfermechanical engineeringthermal engineeringadditive manufacturingmanufacturingengineering optimization

Investigation of the Effects of Geometry Variations on the Performance of an Adjoint Optimized Film Cooling Hole. Heat Transfer (2024)

Molly E. EllingerElise M. FlachsDavid G. Bogard

Overall Cooling Effectiveness With Internal Serpentine Channels and Optimized Film Cooling Holes. Journal of Turbomachinery (2024)

Christopher YoonElise M. FlachsMolly E. EllingerDavid G. Bogard

internal serpentine channelsengineeringheat transfermechanical engineeringthermal engineeringturbomachinery

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2
3
4
5
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10 / page

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supersonic combustion

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