The high-temperature non-equilibrium effect is a novel and significant issue in the flows over
a high Mach number (above Mach 8) air-breathing vehicle. Thus, this study attempts to …

To compromise the compression efficiency and the starting properties, the inner contraction
ratio (ICR) of a general high Mach number inlet is usually designed in the range of dual …

Numerical simulation of hypersonic intake starting characteristics is presented. Three
dimensional RANS equations are solved alongwith SST turbulence model using commercial …

Self-starting ability defines the operational envelope of a hypersonic inlet. To demonstrate
the feasibility of enlarging the self-starting operational envelope using a splitter, numerical …

The starting of a supersonic air-intake at the design Mach number depends on the internal
blockage due to flame-holder struts in the combustor. In the present work, the starting of a …

Isolator flows downstream of the scoop model inlet were visualized by using a planar laser
Rayleigh scattering imaging technique. The scoop model was designed for a cruise Mach …

Numerical simulations were carried out to study the unsteady flow in an intake of hypersonic
air-breathing vehicle. Unsteady RANS simulations were performed to examine started flow …

The numerical simulation of a typical 2D supersonic inlet is carried out to study the effects of
the bleed position in the internal contraction section on the self-starting performance and …

The fixed geometric inlet only has better performance near the design Mach number, and it
is difficult to meet the demand of the combined cycle engine. A multistage adjustable …

В статье приводятся данные численного определения рабочих характеристик
сверхзвукового воздухозаборного устройства с центральным телом в пакете …