Simulation of Laser-Induced Plasma Ignition in a Hypersonic Crossflow
Author:
Affiliation:
1. The University of Queensland, Brisbane, Queensland 4072, Australia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J055821
Reference27 articles.
1. Operability Benefits of Airbreathing Hypersonic Propulsion for Flexible Access to Space
2. Orbital Delivery of Small Payloads Using Hypersonic Airbreathing Propulsion
3. How Much Compression Should a Scramjet Inlet Do?
4. Dynamics of H2O Temperature and Concentration in Zone of Plasma-Assisted High-Speed Combustion
5. Plasma assisted flame ignition of supersonic flows over a flat wall
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