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Engineering Commons

Open Access. Powered by Scholars. Published by Universities.®

Aerospace Engineering

Air Force Institute of Technology

2018

Gas turbines

Articles 1 - 2 of 2

Full-Text Articles in Engineering

Investigation Of Geometric And Thermal Scaling Effects On Simulated Turbine Vane Leading Edge Model, James G. Tewaheftewa Mar 2018

Investigation Of Geometric And Thermal Scaling Effects On Simulated Turbine Vane Leading Edge Model, James G. Tewaheftewa

Theses and Dissertations

Film cooling is still a bustling research topic, especially with burgeoning manufacturing techniques on the horizon that will open the design space. However, despite the number of years that have gone into gas turbine design and research, evaluating cooling performance on components still presents challenges. This task becomes especially difficult and dangerous if trying to do so in realistic engine conditions. Therefore, the majority of film cooling research is performed at conditions far from realistic engine conditions, often using materials that would never hold up to turbine inlet temperature, and scaled to predict results at engine conditions. Previous film cooling …


Influence Of Coolant Flow Rate Parameters In Scaling Gas Turbine Cooling Effectiveness On A Flat Plate, Jacob P. Fischer Mar 2018

Influence Of Coolant Flow Rate Parameters In Scaling Gas Turbine Cooling Effectiveness On A Flat Plate, Jacob P. Fischer

Theses and Dissertations

Effective film cooling relies on the performance of the selected cooling hole shape and placement of the holes on the surface of the blade. To test each holes effectiveness, large scale, low-temperature testing has been used to reduce cost and complexity. The resulting quantity from this testing is called the adiabatic effectiveness (n). The adiabatic effectiveness can then scaled up to engine operating conditions to predict how the selected film cooling hole will perform. This process is complicated by the nonlinear variation of gas properties between coolant and freestream conditions as well as between the experimental and engine conditions. In …