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Investigation of an approximately 0.178-chord-thick NACA 6-series-type airfoil section equipped with sealed internally balanced 0.20-chord ailerons and with a 0.05-chord tab / by Visconti, Fioravante
Published 1948Call Number: Loading…
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2
Further experimental studies of area suction for the control of the laminar boundary layer on a porous bronze NACA 64A010 airfoil / by Braslow, Albert L.
Published 1950Other Authors: “…Visconti, Fioravante…”
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3
Investigation of boundary-layer Reynolds number for transition on an NACA 65₍₂₁₅₎-114 airfoil in the Langley two-dimensional low-turbulence pressure tunnel / by Braslow, Albert L.
Published 1948Other Authors: “…Visconti, Fioravante…”
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4
Thirty-seventh annual report of the National Advisory Committee for Aeronautics. 1951. Including technical reports nos. 1003 to 1058
Published 1952Other Authors:Call Number: Loading…Online Access
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