An Experimental and Computational of Low Re Number Transitional Flows over an Aerofoil with Leading Edge Slat

M S Genc, Gary Lock, U Kaynak

Research output: Contribution to conferencePaperpeer-review

Original languageEnglish
Publication statusPublished - 14 Sept 2008
Event8th AIAA Aviation, Technology and Operation Conference - Alaska, USA United States
Duration: 14 Sept 200819 Sept 2008

Conference

Conference8th AIAA Aviation, Technology and Operation Conference
Country/TerritoryUSA United States
CityAlaska
Period14/09/0819/09/08

Bibliographical note

AIAA Paper 2008-8877

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