An Asymptotic Solution for the Centre of a Rolled-up Conical Vortex Sheet in Compressible Flow-Reference-Cited by-同舟云学术

An Asymptotic Solution for the Centre of a Rolled-up Conical Vortex Sheet in Compressible Flow

Published:1967-11 Issue:4 Volume:18 Page:354-366
ISSN:0001-9259
Container-title:Aeronautical Quarterly
language:en
Short-container-title:Aeronautical Quarterly

Author:

Brown Susan N.,Mangler K. W.

Abstract

SummaryThe asymptotic solution, valid near the centre of a rolled-up vortex sheet, obtained by Mangier and Weber, is generalised to include the effects of compressibility. The vortex sheet is taken to be embedded in a potential flow, and the flow field is assumed to be conical.

Publisher

Cambridge University Press (CUP)

Subject

General Engineering

Reference8 articles.

1. A theory of the flow past a slender delta wing with leading edge separation

2. Smith J. H. B. Improved calculations of leading-edge separation from slender delta wings. RAE Tech. Report 66070, 1966.

3. A theory for the core of a leading-edge vortex

4. Mangler K. W. and Sells C. C. L. The flow field near the centre of a slender rolled-up conical vortex sheet. RAE Tech. Report 67029, 1967.

5. The compressible inviscid leading-edge vortex

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