Vortex formation and flow separation: the beauty and the beast in aerodynamics

Author:

Elsenaar A.

Abstract

Ladies and gentlemen, it is an honour and a great pleasure to present this Lanchester Memorial Lecture. I thank the Royal Aeronautical Society and its Aerodynamic Committee for inviting me. In preparing this lecture I greatly enjoyed the added significance of presenting it in the historical context set by Lanchester. But the real pleasure is to be here among many good friends with whom I worked together for shorter or longer periods.“A body that in its motion through a fluid does not give rise to a surface of discontinuity.” So Lanchester defined a ‘ streamline body’ in his standard work Aerodynamics. With ‘ discontinuity’ the boundary is meant between the outer flow and the dead water region formed by fluid that departs from the surface as illustrated nicely in Fig. 1 for the flow around a cylinder.

Publisher

Cambridge University Press (CUP)

Subject

Aerospace Engineering

Reference49 articles.

1. Legendre R. Écoulement au voisinage de la pointe avant d'une aile à flèche aux incidences moyennes, 1952, 8th Int Cong Th Appl Mech, Istanbul.

2. 27th Lanchester Memorial Lecture scale effect in transonic flow

3. Smith J.H.B. Behaviour of a vortex sheet separating from a smooth surface, RAE TR-77058, 1977.

4. Smith J.H.B. Vortical flows and their computation, 1980, RAE Tech Memo AERO, 1866.

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