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Chief Characteristics and Advantages of Tailless AirplanesThis study will be concerned with the critical examination of two main questions, mainly, susceptibility of centering and more generally, the conditions of static stability, longitudinal equilibrium, and the question of dynamic stability, or at least the damping of longitudinal vibrations about a position of equilibrium that may result from a small variation in the angle of attack.
Document ID
19930094623
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Dufaure De Lajarte, A
Date Acquired
September 6, 2013
Publication Date
May 1, 1936
Report/Patent Number
NACA-TM-794
Accession Number
93R23543
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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