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Flight Studies of the Horizontal-Tail Loads Experienced by a Fighter Airplane in Abrupt ManeuversField measurements were made on a fighter airplane to determine the approximate magnitude of the horizontal tail loads in accelerated flight. In these flight measurements, pressures at a few points were used as an index of the tail loads by correlating these pressures with complete pressure-distribution data obtained in the NACA full-scale tunnel. In addition, strain gages and motion pictures of tail deflections were used to explore the general nature and order of magnitude of fluctuating tail loads in accelerated stalls.
Document ID
19930091869
Acquisition Source
Legacy CDMS
Document Type
Other
Date Acquired
September 6, 2013
Publication Date
January 1, 1944
Report/Patent Number
NACA-TR-792
Accession Number
93R21159
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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