NASA Technical Reports Server (NTRS) 19930090816: The span as a fundamental factor in airplane design

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Title
NASA Technical Reports Server (NTRS) 19930090816: The span as a fundamental factor in airplane design
Publication year listed
1928
Format
Public domain eBook
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NASA Technical Reports Server (NTRS) 19930090816: The span as a fundamental factor in airplane design

Author: NASA Technical Reports Server (NTRS)

Year: 1928

Previous theoretical investigations of steady curvilinear flight did not afford a suitable criterion of "maneuverability," which is very important for judging combat, sport and stunt-flying airplanes. The idea of rolling ability, i.e., of the speed of rotation of the airplane about its X axis in rectilinear flight at constant speed and for a constant, suddenly produced deflection of the ailerons, is introduced and tested under simplified assumptions for the air-force distribution over the span. This leads to the following conclusions: the effect of the moment of inertia about the X axis is negligibly small, since the speed of rotation very quickly reaches a uniform value.

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