Criterion for spanwise spacing of stall cells

Andreas Gross, Hermann F. Fasel, Michael Gaster

Research output: Contribution to journalArticle

10 Scopus citations

Abstract

An explanation for the appearance of stall cells based on lifting-line theory is offered and a simple formula for estimating the stall cell spacing is derived. As the angle of attack is increased beyond the stall angle a recirculation region forms near the trailing edge. The present analysis considers the entire flow region, both over the airfoil and the separated flow region. A model is developed for an infinite-span rectangular wing based on lifting-line theory.

Original languageEnglish (US)
Pages (from-to)272-275
Number of pages4
JournalAIAA journal
Volume53
Issue number1
DOIs
StatePublished - Jan 1 2015

    Fingerprint

ASJC Scopus subject areas

  • Aerospace Engineering

Cite this