Scramjet Nozzle Designed by Chaotic Particle Swarm Optimization and Space-Marching Godunov Scheme
Author:
Affiliation:
1. Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China
Funder
Natural Science Fund of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Reference12 articles.
1. A Century of Ramjet Propulsion Technology Evolution
2. Large eddy simulation of a hydrogen-fueled scramjet combustor with dual cavity
3. Numerical investigation on the ram–scram transition mechanism in a strut-based dual-mode scramjet combustor
4. Influences of Geometric Parameters upon Nozzle Performances in Scramjets
5. Minimum Length Axisymmetric Laval Nozzles
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2. Review on the aerodynamic issues of the exhaust system for scramjet and turbine based combined cycle engine;Progress in Aerospace Sciences;2023-11
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