Effect of thermally induced perturbation in supersonic boundary layers

DOI10.1063/1.3432513zbMath1190.76133OpenAlexW2066620839MaRDI QIDQ3578620

Hong Yan, Datta V. Gaitonde

Publication date: 20 July 2010

Published in: Physics of Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1063/1.3432513

zbMATH Keywords

vorticesturbulencesupersonic flowboundary layers

Mathematics Subject Classification ID

Fluid mechanics (76-XX)

Related Items (1)

Analysis of plasma-based flow control mechanisms through large-eddy simulations

Uses Software

• LASTRAC

Cites Work

• Unnamed Item
• Approximate Riemann solvers, parameter vectors, and difference schemes
• Stability and transition in shear flows
• Towards the ultimate conservative difference scheme. V. A second-order sequel to Godunov's method
• Spatial theory of optimal disturbances in boundary layers
• Receptivity of a boundary-layer flow to a three-dimensional hump at finite Reynolds numbers
• Turbulence measurements in a three-dimensional boundary layer in supersonic flow
• The three-dimensional nature of boundary-layer instability

This page was built for publication: Effect of thermally induced perturbation in supersonic boundary layers