Publication Date:
2011-08-18
Description:
A fundamental analysis of two-dimensional supersonic boundary layer flow, both laminar and turbulent, is presented for a wide range of normal and nonnormal mass-transfer velocities. The analysis is based on the numerical solution of the Navier-Stokes equations, and results are compared with available theoretical and experimental data. Certain cases of practical importance, for which results are not presently available, are referred to.
Keywords:
AERODYNAMICS
Type:
Computer Methods in Applied Mechanics and Engineering; 25; Jan. 198
Format:
text