1954•NASA STI Repository (National Aeronautics and Space Administration)Requires access
Measured and Estimated Lateral Static and Rotary Derivatives of a 1/12-scale Model of a High-speed Fighter Airplane with Unswept Wings
J. L. Williams
Open publisher page 0 citations
Abstract
Report presenting a low-speed investigation to determine the lateral static and rotary derivatives of a model of a high-speed fighter airplane. The purpose was to compare experimental stability derivatives with derivatives estimated for a wing-fuselage combination, a vertical- and horizontal-tail combination, and a complete model.