Measurement of the Dynamic Lateral Stability of the Douglas D-558-1 Airplane (Buaero No. 37971) in Rudder Kicks at a Mach Number of 0.72

In the course of a stability and control investigation of the D-558--1 airplane, rudder kicks were made at a Mach number of 0.72 at a pressure altitude of 8500 feet. The lateral oscillations resulting from the rudder kicks required 1 1/2 seconds to damp to half amplitude and had a period of 1.1 seco...

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Bibliographische Detailangaben

1. Verfasser:	Drake, Hubert M
Format:	Report
Sprache:	eng
Schlagworte:	Aerodynamics
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