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A Comparison of the Lateral Motion Calculated for Tailless and Conventional AirplanesTheoretical analysts of lateral dynamic motion of tailless and conventional airplanes was made for fighter and heavy transport. Their reactions to a lateral gust and control power required by each for simple maneuvers were determined and compared. Both types of airplanes require almost identical aileron control power to perform a given maneuver; tailless airplane requires about 1-2 to 1-3 directional control power of conventional airplane. Tailless airplane also shows greatest displacement for a given disturbance and has least damping in oscillatory mode.
Document ID
19930081822
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Technical Note
External Source(s)
Authors
Harper, Charles W.
(National Advisory Committee for Aeronautics. Ames Aeronautical Lab. Moffett Field, CA, United States)
Jones, Arthur L.
(National Advisory Committee for Aeronautics. Ames Aeronautical Lab. Moffett Field, CA, United States)
Date Acquired
August 16, 2013
Publication Date
February 1, 1947
Subject Category
Aerodynamics
Report/Patent Number
NACA-TN-1154
Report Number: NACA-TN-1154
Accession Number
93R11112
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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