高超声速飞行器绕流存在着激波, 边界层, 流动分离, 稀薄气体效应和高温气体效应等多种复杂
流动现象的空气动力学问题, 其中高超声速边界层转捩既是空气动力学的基础问题 …

I. Nomenclature αi= amplification rates [m-1] P= Pressure [Pa] f= frequency [kHz] Re=
Reynolds number PSD= Power Spectral Density [Pa2/Hz] L= Length of hollow cylinder [m] …

In the present study, three boundary-layer stability codes are compared based on
hypersonic high-enthalpy boundary-layer flows around a blunted 7 deg half-angle cone. The …

In this paper, we present a methodology to achieve high-fidelity simulations of chemically
reacting hypersonic flows and demonstrate our numerical solver's capabilities on a selection …

The instability and transition of hypersonic boundary layer on a blunted delta wing is
performed by numerical simulation of experiments conducted in the quiet wind tunnel …

Hypersonic flows are of great interest in a wide range of aerospace applications and are a
critical component of many technological advances. In this thesis, we first numerically study …