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August 17, 2025

Design and Fabrication of a Thermally Optimized Gas Turbine Nozzle

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Authors

EFElise M. FlachsDBDavid G. Bogard

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Overview

Innovative gas turbine nozzle reduces wall temperatures in hydrogen-fueled combustors, highlighting novel cooling strategies.

Key Points

  • The design successfully maintained wall temperatures under Inconel 718's melting point during testing.
  • At engine realistic temperatures of 1750K, the nozzle performance was evaluated using computational and experimental methods.
  • Manufacturing utilized advanced techniques to create complex geometries that enhance cooling efficiency in gaseous environments.
  • This approach holds promise for improving designs in high-heat gas turbine applications across various industries.

Cite This Study

Flachs et al. (2025) studied this question.

synapsesocial.com/papers/68a36f840a429f79733320d4https://doi.org/10.1115/gt2025-153314
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