Adding fuel strut in scramjet combustor is an effective solution to improve fuel-air mixing and
combustion efficiency. However, strut injector suffers from extreme aerodynamic heat …

Regarding future space transportation systems SCRamjets are generally considered a
complement or even an alternative to standard rocket propulsion systems. As the ambient air …

This current work presents the performance analysis of a supersonic combustor interface
and flow construction through a scramjet engine with a planar shaped strut injector (PSSI) at …

The penetration height of fuel from the wall injection in a supersonic combustor of scramjet is
generally low, leading to insufficient fuel/air mixing and low combustion efficiency. A strut …

A parametric study of combustor inlet configuration for supersonic combustion ramjet
(Scramjet) engine has been conducted by solving two-dimensional full Navier–Stokes …

In view of the very high freestream velocity of scramjets reaching Mach 10, fuel residence
time is on the order of milliseconds1 and supersonic combustion presents a challenge in …

The design of the strut fuel injector plays an important role in the performance of the strut-
based scramjet combustor. The current study numerically investigates the flow and …

A detailed numerical analysis on a scramjet combustor is carried out by introducing an
innovative shaped strut in place of the conventional strut. The design of newly added strut …

The strut-based injector has been found to be one of the most promising injector designs for
a supersonic combustor, offering enhanced mixing of fuel and air. The mixing and flow field …

A feasible method was developed for cooling of the extreme aerodynamic heating of strut
injectors in a scramjet engine. A porous strut injector using transpiration cooling was …