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

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

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Background radiation compensation calibration method for film cooling infrared temperature measurement based on BP neural network;International Communications in Heat and Mass Transfer;2024-12

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