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- W28182372 abstract "In this paper, methods for conducting flight tests to determine both the stick-fixed and stick-free stability levels of the airplane are presented. The concepts of the airplane neutral points and maneuver points are discussed and the data reduction processes required to establish these center of gravity positions from flight test data explained. Several different approaches to the problem are examined, including such important methods as measurements of elevator angle and stick force versus airspeed at constant c.g. positions, as well as measurements of airspeed versus c.g. position at constant elevator angle and at zero stick force. The advantages and disadvantages of the different systems are explained and the flight test technique described in each case. The analysis of the trim curves for by-products such as elevator power (dCm/dδe) and stability criterion (dCm/dCL) is explained. Methods for testing for control limitations in take-off and landing are described, and finally, tests for changes in trim, due to variations in flaps and power settings are presented." @default.
- W28182372 created "2016-06-24" @default.
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- W28182372 date "1959-01-01" @default.
- W28182372 modified "2023-09-26" @default.
- W28182372 title "STATIC LONGITUDINAL STABILITY AND CONTROL" @default.
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- W28182372 doi "https://doi.org/10.1016/b978-1-4831-9730-2.50012-0" @default.
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