Work

Elevated Mainstream Mach Number Effects on Shaped Gas Turbine Film Cooling Holes

Year: 2025

Type: article

Source: Journal of Turbomachinery

DOI: 10.1115/1.4069945

Authors: Michael T. Furgeson, Elise M. Flachs, David G. Bogard

Institution: The University of Texas at Austin

Language: English

Topic: Turbomachinery Performance and Optimization

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

Funder: U.S. Department of Energy

Award: DE-FE0031760 UNIVERSITY OF TEXAS AT AUSTIN UNIVERSITY TURBINE SYSTEMS RESEARCH (UTSR) INTEGRATED TURBINE COMPONENT COOLING DESIGNS FACILITATED BY ADDITIVE MANUFACTURING AND OPTIMIZATION

OpenAlex ID: W4414501335

FWCI: 1.199

Cites: 20

Cited by: 3

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