Development of Dynamic Discharge Arc Driver with Computer-Aided Circuit Simulation
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, Calif.
2. University of Split, Split, Yugoslavia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference17 articles.
1. A higher performance electric-arc-driven shock tube
2. A conical arc driver for high-energy test facilities.
3. Arc Driver Operation for Either Efficient Energy Transfer or High-Current Generation
Cited by 5 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. Studies of non-equilibrium radiation signatures behind hypersonic shock fronts;27th Thermophysics Conference;1992-07-06
2. An overview of Ames experimental aerothermodynamics;Shock Waves;1992
3. Operating characteristics of a 60- and 10-cm electric arc-driven shock tube. I - The driver. II - The driven section;Journal of Thermophysics and Heat Transfer;1990-07
4. Unsteady gas dynamic model of an arc-heated shock;AIAA Journal;1981-06
5. Transient solution for megajoule energy release in a lumped‐parameter series RLC circuit;Journal of Applied Physics;1980-01
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