Mesh-refined computation of disordered vortex flow around a cranked delta wing: Transonic speed-Reference-Cited by-同舟云学术

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Mesh-refined computation of disordered vortex flow around a cranked delta wing: Transonic speed

Published:1988-03 Issue:2 Volume:4 Page:189-195
ISSN:0748-8025
Container-title:Communications in Applied Numerical Methods
language:en
Short-container-title:Commun. appl. numer. methods

Author:

Rizzi Arthur,Purcell Charles J.

Publisher

Wiley

Subject

General Engineering

Reference18 articles.

1. ‘Numerical computation of vortical flows about wings’, NLR Report MP 83073 U, Amsterdam (1983).

2. ‘Theoretical modelling of three-dimensional vortex flows in aerodynamics’. Aero J., April, pp. 101-116 (1984).

3. The stability of an expanding circular vortex sheet

4. The stability of an evolving two‐dimensional vortex sheet

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