Geometric parameters measurement for the multi-view internal fusion morphology of turbine blade cooling holes-Reference-Cited by-同舟云学术

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Geometric parameters measurement for the multi-view internal fusion morphology of turbine blade cooling holes

Published:2024-04 Issue: Volume:175 Page:108038
ISSN:0143-8166
Container-title:Optics and Lasers in Engineering
language:en
Short-container-title:Optics and Lasers in Engineering

Author:

Li Lei^ORCID,Li Bing,Xue Zhangfeng,Xin Meiting,Wei Xiang^ORCID

Publisher

Elsevier BV

Subject

Electrical and Electronic Engineering,Mechanical Engineering,Atomic and Molecular Physics, and Optics,Electronic, Optical and Magnetic Materials

Reference40 articles.

1. The hotter the engine, the better;Perepezko;Science,2009

2. Film-cooling performance of converged-inlet hole shapes;Kim;Int. J. Therm. Sci.,2018

3. Film cooling of showerhead holes from the twisted leading edge of a gas turbine blade: Complex mainstream characteristics and reasonable angle arrangement;Zhao;Aerosp. Sci. Technol.,2021

4. Film cooling performance on pressure side of turbine blade with different number of hole rows under rotating state;Meng;Aerosp. Sci. Technol.,2022

5. Asme, Effects of coolant feed direction on additively manufactured film cooling holes;Stimpson,2018

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