Direct simulation Monte Carlo computations and experiments on leading-edge separation in rarefied hypersonic flow

DOI10.1017/jfm.2019.692zbMath1430.76353OpenAlexW2978375336MaRDI QIDQ5235755

No author found.

Publication date: 14 October 2019

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1017/jfm.2019.692

zbMATH Keywords

separated flowsrarefied gas flowhigh-speed flow

Mathematics Subject Classification ID

Supersonic flows (76J20) Hypersonic flows (76K05) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (2)

Shock-induced leading-edge separation in hypersonic flows ⋮ Unified gas-kinetic scheme with simplified multi-scale numerical flux for thermodynamic non-equilibrium flow in all flow regimes

Cites Work

• On the curvature of compressible boundary layer flows near separation
• A Method for the Spatial Discretization of Parabolic Equations in One Space Variable
• Once again on the supersonic flow separation near a corner
• Rates of thermal relaxation in direct simulation Monte Carlo methods
• Predicting failure of the continuum fluid equations in transitional hypersonic flows
• Laminar hypersonic leading edge separation – a numerical study
• Shock Wave-Boundary-Layer Interactions
• Recent Studies of the Laminar Base-Flow Region
• Base pressure in laminar supersonic flow
• Viscous and resistive eddies near a sharp corner
• Unnamed Item
• Unnamed Item

This page was built for publication: Direct simulation Monte Carlo computations and experiments on leading-edge separation in rarefied hypersonic flow