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Airship Model Tests in the Variable Density Wind Tunnel

Experiments With an Airfoil Model on Which the Boundary Layers Are Controlled Without the Use of Supplementary Equipment

The drag of two streamline bodies as affected by protuberances and appendages

Fuselage-drag tests in the variable-density wind tunnel: streamline bodies of revolution, fineness ratio of 5

Tests in the variable-density wind tunnel of the NACA 23012 airfoil with plain and split flaps

Flow observations with tufts and lampblack of the stalling of four typical airfoil sections in the NACA variable-density tunnel

Preliminary Investigation of Certain Laminar-Flow Airfoils for Application at High Speeds and Reynolds Numbers


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