[PDF][PDF] Enlarge duct length optimization for suddenly expanded flows
In many applications like the aircraft or the rockets/missiles, the flow from a nozzle needs to
be expanded suddenly in an enlarged duct of larger diameter. The enlarged duct is provided …
be expanded suddenly in an enlarged duct of larger diameter. The enlarged duct is provided …
Influence of water injection on performance of scramjet engine
Y Xiong, J Qin, K Cheng, Y Wang - Energy, 2020 - Elsevier
In order to investigate the influence of water injection on performance of scramjet engine, a
thermodynamic model with the constant cross sectional area heating process was …
thermodynamic model with the constant cross sectional area heating process was …
Numerical analysis and design optimization of supersonic after-burning with strut fuel injectors for scramjet engines
Scramjets are a class of hypersonic airbreathing engine that offer promise for economical,
reliable and high-speed access-to-space and atmospheric transport. The expanding flow in …
reliable and high-speed access-to-space and atmospheric transport. The expanding flow in …
Modelling a hypersonic single expansion ramp nozzle of a hypersonic aircraft through parametric studies
A Ridgway, AA Sam, A Pesyridis - Energies, 2018 - mdpi.com
This paper aims to contribute to developing a potential combined cycle air-breathing engine
integrated into an aircraft design, capable of performing flight profiles on a commercial scale …
integrated into an aircraft design, capable of performing flight profiles on a commercial scale …
Thrust augmentation optimization through supersonic after-burning in scramjet engine nozzles via surrogate-assisted evolutionary algorithms
Scramjets are a class of hypersonic airbreathing engine that are associated with realizing
the technology required for economical, reliable and high-speed access-to-space and …
the technology required for economical, reliable and high-speed access-to-space and …