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Measured Moments of Inertia of 32 Airplanes

The additional-mass effect of plates as determined by experiments

The Experimental Determination of the Moments of Inertia of Airplanes by a Simplified Compound-Pendulum Method

Wind-tunnel investigation of six shielded total-pressure tubes at high angles of attack: Subsonic speeds

Wind-Tunnel Investigation of a Number of Total Pressure Tubes at High Angles of Attack

Wind-tunnel investigation of a number of total-pressure tubes at high angles of attack: Subsonic speeds

Wind-Tunnel Investigation of a Shielded Total-Pressure Tube at Transonic Speeds

Flight Investigation at Large Angles of Attack of the Static-Pressure Errors of a Service Pitot-Static Tube Having a Modified Orifice Configuration

Wind-Tunnel Investigation of a Number of Total-Pressure Tubes at High Angles of Attack -- Subsonic, Transonic, and Supersonic Speeds

Wind-Tunnel Investigation of a Number of Total-Pressure Tubes at High Angles of Attack: Subsonic, Transonic, and Supersonic Speeds

Measurement of Static Pressure on Aircraft

Measurement of static pressure on aircraft

The measurement of pressure altitude on aircraft

Measurement of Static Pressure on Aircraft

Summary of Methods of Measuring Angle of Attack on Aircraft


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