The restart ability of inlets is significant to the robustness of hypersonic airbreathing vehicles.
Classic starting theories based on the one-dimensional and inviscid flow assumption cannot …

Aimed at diversity of hypersonic flight mission, multi-objective coordinated control of
regeneratively-cooled scramjet engine with two-stage kerosene injection is discussed for …

Inlet unstart is detrimental to hypersonic airbreathing flights. By unstart, we mean the
separation-induced collapse of a supersonic duct flow. The unstart characteristics of a two …

Aimed at diversity of hypersonic flight mission, this paper discusses the multivariable control
of regeneratively-cooled scramjet engine with two-stage kerosene injection for both safety …

The present work aims at numerical methodology development for modeling supersonic
combustion using 8 species, 13 reaction hydrogen-air reaction model. The governing …