Maximum thrust for the rocket-ejector mode of the hydrogen fueled rocket-based combined cycle engine

Conceptual Study of a Combined-Cycle Engine for an Aerospace Plane

Takeshi Kanda, Kenji Kudo · Journal of Propulsion and Power · 2003 · 112 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

Effect of cooling channel geometry on re-cooled cycle performance for hydrogen fueled scramjet

Wen Bao, W-X Zhou, Donghyeon Yu · International Journal of Hydrogen Energy · 2010 · 71 citations

Engineering, Chemical Engineering, Mechanical Engineering +13

Optimal Supersonic Ejector Designs

J. C. Dutton, Bruce Carroll · Journal of Fluids Engineering · 1986 · 68 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

Analysis of combustion mode and operating route for hydrogen fueled scramjet engine

Ruifeng Cao, Juntao Chang, Wen Bao et al. · International Journal of Hydrogen Energy · 2013 · 59 citations

Engineering, Aerospace Engineering, Mechanical Engineering +14

Thermodynamic analysis on specific thrust of the hydrocarbon fueled scramjet

Qingchun Yang, Juntao Chang, Wen Bao · Energy · 2014 · 53 citations

Engineering, Aerospace Engineering, Mechanical Engineering +14