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Some Lift and Drag Measurements of Two Configurations of a Nacelle and Oil-Cooler Scoop for the Hughes-Kaiser Cargo Airplane

Tests of the NACA 653-018 airfoil section with boundary-layer control by suction

Effects of Reynolds Number and Leading-Edge Roughness on Lift and Drag Characteristics of the NACA 653-418, a=1.0 Airfoil Section

Summary of Data Relating to the Effects of Wing Machine-Gun and Cannon Installations on the Aerodynamic Characteristics of Airplanes

Wind-Tunnel Investigation of Boundary-Layer Control by Suction on the NACA 653-418, a = 1.0 Airfoil Section with a 0.29-Airfoil-Chord Double Slotted Flap

Summary of Drag Characteristics of Practical-Construction Wing Sections

Tests of the NACA 64(SUB 1)A212 airfoil section with a slat, a double slotted flap, and boundary-layer control by suction

Summary of drag characteristics of practical-construction wing sections

Wind-tunnel investigation of the NACA 654-421 airfoil section with a double slotted flap and boundary layer control by suction

Drag Tests of an NACA 65(215)-114, a = 1.0 Practical-Construction Airfoil Section Equipped with a 0.295-Airfoil-Chord Slotted Flap


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