The boundary layer that develops at the lower wing surface of a very sweptback wing and an incident wing was analyzed. The analysis is part of a general study of flow in the angle formed by two intersecting walls.
Analyse de la Couche Limite a l'Intrados d'une Aile en Fleche et en Incidence (Analysis of the Boundary Layer at the Lower Wing Surface of Sweptback and Incident Wings)
1988
65 pages
Report
Keine Angabe
Englisch
Europäisches Patentamt | 2019
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