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Investigation into Scale Effects on the Performance of Sub Boundary-Layer Vortex Generators on Civil Aircraft High-Lift Devices

Publikation: PaperBegutachtung

7 Zitate (Scopus)
OriginalspracheEnglish
PublikationsstatusPublished - Juni 2002
Veranstaltung1st American Institute of Aeronautics and Astronautics (AIAA) Flow Control Conference - St Louis, United States
Dauer: 24 Juni 200226 Juni 2002

Conference

Conference1st American Institute of Aeronautics and Astronautics (AIAA) Flow Control Conference
Land/GebietUnited States
OrtSt Louis
Zeitraum24/06/0226/06/02

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