Hostname: page-component-cd9895bd7-fscjk Total loading time: 0 Render date: 2024-12-18T19:20:50.657Z Has data issue: false hasContentIssue false

Photographic evidence of the formation and growth of vorticity behind plates accelerated from rest in still air

Published online by Cambridge University Press:  28 March 2006

D. Pierce
Affiliation:
Aerodynamics Department, Royal Aircraft Establishment, Farnborough, Hampshire, England

Abstract

The shedding of vorticity from the edges of a plate, which is accelerated normal to itself from rest in still air, is investigated experimentally by means of a new flow-visualization technique using spark-lighted shadowgraphs and heated air, benzene or other vapours to introduce sufficient changes in density along the surface of discontinuity.

The photographs show small-scale undulations and the formation of a number of centres of vorticity along the well known big-scale vortex sheets which roll up along their edges.

Type
Research Article
Copyright
© 1961 Cambridge University Press

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

Footnotes

Crown copyright reserved.

References

Anton, L. 1939 Formation of a vortex at the edge of a plate. Ing. -Arch. 10, 411.Google Scholar
Bollay, W. 1937 A theory for rectangular wings of small aspect ratio. J. Aero. Sci. 4, 294.Google Scholar
Bollay, W. 1939 A non-linear wing theory and its application to rectangular wings of small aspect ratio. Z. angew. Math. Mech. 19, 21.Google Scholar
Hall, M. G. 1961 A theory for the core of a leading edge vortex. J. Fluid Mech. 11, 209.Google Scholar
Küchemann, D. 1955 A non-linear lifting surface theory for wings of small aspect ratio with edge separations. Aero. Res. Counc., Rep. no. 17,769.Google Scholar
Mangler, K. W. 1939 Der kleinste induzierte Widerstand eines Tragflügels mit kleinem Seitenverhältnis. Jb. dtsch. Luftfahrt, 1, 140.Google Scholar
Mangler, K. W. & Smith, J. H. B. 1959 A theory of the flow past a slender delta wing with leading edge separation. Proc. Roy. Soc. A, 251, 200.Google Scholar
Prandtl, L. 1904 Über Flüssigkeitsbewegung bei sehr kleiner Reibung. Verhandlungen des III. Internationalen Mathematiker-Kongresses, Heidelberg. (Leipzig: B. G. Teubner, 1905.)
Wedemeyer, E. 1956 Ausbildung eines Wirbelpaares an den Kanten einer Platte. Max-Planck-Institut für Strömungsforschung, Bericht, 56/B/06.
Wille, R. 1960 Modellvorstellungen zumübergang Laminar-Turbulent. Deutsche Versuchsanstalt für Luftfahrt E. V. Bericht, Nr. 113.