Modelling dynamic stall vortex inception at low Mach numbers

A. J. Niven, R. A.Mc D. Galbraith

Research output: Contribution to specialist publicationArticle

Abstract

Results of a comparison of dynamic stall onset are presented, as assessed from low Mach number windtunnel data contained in the University of Glasgow's database and that from the well established Beddoes' model. The model, which was originally developed to reconstruct higher Mach number dynamic stall characteristics, exhibited a lower stall onset incidence than that assessed from the windtunnel data. The differences and speculations on the physical reasoning underlying the two assessments are discussed. An addition to the Beddoes model is proposed which yields an improved reconstruction of the Glasgow windtunnel data.

Original languageEnglish
Pages67-76
Number of pages10
Volume101
No.1002
Specialist publicationAeronautical Journal
Publication statusPublished - Feb 1997

Fingerprint

Dive into the research topics of 'Modelling dynamic stall vortex inception at low Mach numbers'. Together they form a unique fingerprint.

Cite this