The compressible laminar boundary layer with foreign gas injection

Date

1962-01

Free to read from

Supervisor/s

Journal Title

Journal ISSN

Volume Title

Publisher

College of Aeronautics

Department

Type

Report

ISSN

Format

Citation

Abstract

The equations of the steady compressible two-dimensional laminar boundary layer with foreign gas injection through a porous wall are solved, using an extended form of Lighthill's approximate method, for arbitrary main stream pressure gradient, wall temperature and injection velocity. The wall shear stress and heat transfer rate are obtained in the form of equations suitable for iteration. It is shown that substantial reductions in skin friction and heat transfer rate can be obtained by the injection of a light gas instead of air.

Description

Software Description

Software Language

Github

Keywords

DOI

Rights

Relationships

Relationships

Supplements

Funder/s

Collections