The paper describes a numerical investigation of linear and nonlinear instability in high-speed boundary layers. Both a frozen gas and a finite-rate chemically reacting gas are considered. The weakly nonlinear instability in the presence of a large-amplitude two-dimensional wave is investigated for the case of fundamental resonance. Depending on the amplitude of this two-dimensional primary wave, strong growth of oblique secondary perturbations occurs for favourable relative phase differences between the two. For essentially the same primary amplitude, secondary amplification is almost identical for a reacting and a frozen gas. Therefore, chemical reactions do not directly affect the growth of secondary perturbations, but only indirectly th...
International audienceThe influence of high-enthalpy effects on hypersonic turbulent boundary layers...
The effect of Mach number on the growth of unstable disturbances in a boundary layer undergoing a st...
University of Minnesota Ph.D. dissertation. May 2012. Major: Aerospace Engineering and Mechanics. Ad...
The paper describes a numerical investigation of linear and nonlinear instability in high-speed boun...
Prediction of laminar-turbulent transition is a key factor in the design of the heat shield of vehic...
Laminar-turbulent transition prediction in hypersonic boundary layer remains one of the most challen...
© © 2014 Cambridge University Press.Nonlinear instability in a supersonic boundary layer at Mach 4.8...
The future of space exploration and commercial space travels relies on the development of high-perfo...
The linear and weakly nonlinear transition regime of a hypersonic boundary layer on a sharp cone wit...
Advancing towards the correct modeling and subsequent understanding of laminar-to-turbulenttransitio...
Three dimensional linear secondary instability theory is extended for compressible boundary layers o...
Linear and weakly nonlinear stages of the laminar-to-turbulent transition process are investigated i...
The purpose of this work is to shed light on the role of chemical equilibrium in the global instabil...
An experimental campaign was conducted at the University of Maryland - College Park to examine the i...
Copyright © 2014 Zhenqing Wang et al.This is an open access article distributed under theCreative Co...
International audienceThe influence of high-enthalpy effects on hypersonic turbulent boundary layers...
The effect of Mach number on the growth of unstable disturbances in a boundary layer undergoing a st...
University of Minnesota Ph.D. dissertation. May 2012. Major: Aerospace Engineering and Mechanics. Ad...
The paper describes a numerical investigation of linear and nonlinear instability in high-speed boun...
Prediction of laminar-turbulent transition is a key factor in the design of the heat shield of vehic...
Laminar-turbulent transition prediction in hypersonic boundary layer remains one of the most challen...
© © 2014 Cambridge University Press.Nonlinear instability in a supersonic boundary layer at Mach 4.8...
The future of space exploration and commercial space travels relies on the development of high-perfo...
The linear and weakly nonlinear transition regime of a hypersonic boundary layer on a sharp cone wit...
Advancing towards the correct modeling and subsequent understanding of laminar-to-turbulenttransitio...
Three dimensional linear secondary instability theory is extended for compressible boundary layers o...
Linear and weakly nonlinear stages of the laminar-to-turbulent transition process are investigated i...
The purpose of this work is to shed light on the role of chemical equilibrium in the global instabil...
An experimental campaign was conducted at the University of Maryland - College Park to examine the i...
Copyright © 2014 Zhenqing Wang et al.This is an open access article distributed under theCreative Co...
International audienceThe influence of high-enthalpy effects on hypersonic turbulent boundary layers...
The effect of Mach number on the growth of unstable disturbances in a boundary layer undergoing a st...
University of Minnesota Ph.D. dissertation. May 2012. Major: Aerospace Engineering and Mechanics. Ad...