A hypersonic inlet/isolator acts as the “compressor” for scramjet engines through a series of
shocks, which induces complex internal flows. This paper comprehensively reviews the …

This paper proposed the physical information residual spatial pyramid pooling (PIResSpp)
convolutional neural network that is highly robust and introduces a residual neural network …

When integrated with supersonic/hypersonic flight vehicles the ramp shock/boundary layer
interaction occurs in streamline-traced inward-turning inlets exhibit complex three …

For the integrated design of the forebody and hypersonic inlet, the non-uniform inflows
generated by the forebody have significant impacts on the inlet performance. Traditional …

The design of an inward-turning high-speed three-dimensional streamline-traced intake is
presented from osculating axisymmetric theory. To satisfy the osculating intake design …

The prespecified flowfield is essential in the inverse design method for generating inward-
turning streamline-traced intakes, ie, the parent flowfield. The internal conical flow C (ICFC) …

The efficient design of air intake is crucial for high-speed airbreathing propulsion systems.
This paper presents a novel design method that integrates the recently introduced internal …

The current work evaluates the effectiveness of the pressure-corrected osculating
axisymmetric flows method in the design of hypersonic wavecatcher intakes with shape …

A computational tool named SUPIN is being developed to design and analyze the
aerodynamic performance of supersonic inlets. The inlet types available include the …

This study investigates the off-design characteristics of a scoop-type streamline-tracing inlet,
focusing on identifying its operable envelope using numerical and experimental methods …