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Albert L Braslow

Albert L Braslow

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5.
Comparison of the Drag of a Fin-Stabilized Body of Revolution and of a Complete Airplane Configuration as Obtained at Transonic Speeds in a Slotted Wi
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6.
Wind-Tunnel Investigation of Aileron Effectiveness of 0. 20 Airfoil-Chord Plain Ailerons of True Airfoil Contour on NACA 652-415, 653-418 and 654-421 Airfoil Sections (Classic Reprint)NR
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