Aerodynamic losses and heat transfer for a covered trailing edge turbine vane with a high solidity low pressure drop predestal pin fin array and variable coolant ejection

Author

• Indrajit Jaswal

Date of Award

1-1-2008

Document Type

Thesis

Degree Name

Master of Science (MS)

Department

Mechanical Engineering

Recommended Citation

Jaswal, Indrajit, "Aerodynamic losses and heat transfer for a covered trailing edge turbine vane with a high solidity low pressure drop predestal pin fin array and variable coolant ejection" (2008). Theses and Dissertations. 12803.
https://commons.und.edu/theses/12803