Progress in Research on High Speed Flow

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Publication date: 1 December 1955

Abstract

IN the first of these articles it was pointed out that normal supersonic flow can be described theoretically, to a first approximation, by the linearized equation of motion. This has the form of the wave equation and governs first order disturbances to fields of uniform flow; for example, flow past thin wings or slender bodies at small angles of incidence, and flow through ducts of varying cross‐section. In the same way small disturbances in a purely subsonic stream can be described by a linearized equation of motion, which can be reduced to Laplace's equation by contracting the co‐ordinate normal to the direction of flow. Transonic flow, in which regions of both supersonic and subsonic flow occur, is not so easily represented.

Citation

Holt, M. (1955), "Progress in Research on High Speed Flow", Aircraft Engineering and Aerospace Technology, Vol. 27 No. 12, pp. 392-395. https://doi.org/10.1108/eb032632

Download as .RIS

Publisher

:

MCB UP Ltd

Copyright © 1955, MCB UP Limited

Please note you might not have access to this content

You may be able to access this content by login via Shibboleth, Open Athens or with your Emerald account.
If you would like to contact us about accessing this content, click the button and fill out the form.
To rent this content from Deepdyve, please click the button.