In this paper, we present a rigorous numerical approach for the electromagnetic (EM)
analyses of a hypersonic object with plasma sheath. First, the effective EM parameters of the …

The hypersonic flight regime is conventionally defined for Mach> 5; in these conditions, the
flying object becomes enveloped in a plasma. This plasma is densest in thin surface layers …

A new electromagnetic (EM) calculation model, the inhomogeneity zonal medium model
(IZMM)(based on the physical optics (PO) method), is proposed to calculate and analyze the …

Based on the detection platform of space-borne radar (SBR), the dynamic electromagnetic
(EM) scattering characteristics of a hypersonic vehicle covered with plasma sheath are …

This paper presents numerical results in hypersonic aerothermodynamics, a critical field
within aerospace engineering, traditionally focusing on reentry capsules and more recently …

In this article, a hypersonic target electromagnetic (EM) scattering echo model combined
with the inhomogeneous zonal medium model (IZMM) and the classical scattering center …

A novel volumetric shooting and bouncing ray (VSBR) method is first proposed to analyze
the electromagnetic scattering from in-homogeneous plasma sheath. The propagation of …

During reentry, the high temperatures experienced by near-space hypersonic vehicles result
in surface ablation, generating ablative particles. These particles become part of a plasma …

The plasma sheath during reentry of hypersonic vehicle is an unmagnetized and weakly
ionized nonuniform plasma flow, which causes radio frequency blackout and strong plasma …

The hypersonic flow field around a reentry vehicle has a significant influence on the ground‐
vehicle communication as well as on the detection and recognition of the reentry vehicle …