Analysis of the characteristics of scramjet mode and ramjet mode of axisymmetric dual-combustion ramjet
Author:
Funder
National Natural Science Foundation of China
Taizhou Municipal Science and Technology Bureau
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference37 articles.
1. Integral-rocket dual-combustion ramjets: a new propulsion concept;Billig;J. Spacecraft Rockets,1980
2. Supersonic combustion in air-breathing propulsion systems for hypersonic flight;Urzay;Annu. Rev. Fluid Mech.,2018
3. Dual combustor ramjet engine dynamics modeling and simulation for design analysis;Wadwankar,2019
4. Mixing efficiency of hydrogen and air co-flow jets via wedge shock generator in dual-combustor ramjet;Jiang;Aerosp Sci Technol.,2021
5. Freejet experimental investigation on performance of dual-combustion ramjet;Tan;J. Propul. Power,2015
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