Development and Characterization of an Inductively Coupled Plasma Jet for High-Temperature Testing-Reference-Cited by-同舟云学术

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Development and Characterization of an Inductively Coupled Plasma Jet for High-Temperature Testing

Published:2024-01-04 Issue: Volume: Page:
ISSN:
Container-title:AIAA SCITECH 2024 Forum
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Author:

Jarrel Landon B.¹,Brocker Michael T.¹,Williams Aimee¹,Dec John¹,Ahuja Krishan K.¹

Affiliation:

1. Georgia Institute of Technology College of Engineering

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2024-1401

Reference19 articles.

1. Aerothermodynamic design of an inductively coupled plasma wind tunnel

2. A Study of Inductively Coupled Plasma Torch Configurations

3. Principles of Plasma Discharges and Materials Processing

4. Development of a 30kW Inductively Coupled Plasma Torch for Aerospace Material Testing

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. HyperMATE: A Novel Aerothermal Testing Facility at the University of Tennessee;Journal of Thermal Science and Engineering Applications;2024-08-29

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