A note on the description of an attached supersonic boundary layer near a point of injection cut-off

DOI10.1017/S0022112075002674zbMath0311.76035OpenAlexW2139930431MaRDI QIDQ4070930

A. F. Amr, David R. Kassoy

Publication date: 1975

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

Full work available at URL: https://doi.org/10.1017/s0022112075002674

Mathematics Subject Classification ID

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

Cites Work

• Boundary layer separation due to mass addition
• Boundary-Layer Flow Near the Trailing Edge of a Flat Plate

This page was built for publication: A note on the description of an attached supersonic boundary layer near a point of injection cut-off