On the flow along swept leading edges
1965
13 S., [5] Bl
Ill., graph. Darst
Langzeitarchivierung durch Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
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Transition on swept leading edges at Mach 3.5
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Transition on swept leading edges at Mach 3.5
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Numerical Investigations of Vortical Flow on Swept Wings with Round Leading Edges
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Relaminarization on swept leading edges under high-lift conditions
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