How methods for treating servo systems influenced by stochastic disturbances can be applied to aerodynamic problems of stochastic nature, and to make estimation of root mean square deviations of velocity, attitude angles, and load factor of aircraft in straight level flight subjected to normal atmospheric wind disturbances.
Investigation of response to random wind gusts of typical subsonic fighter aircraft in level flight with Mach number 0.9 at sea level
Stockholm. Kungl Tekniska Hogskolans Handlinger (Roy Inst Technology) KTH Aero Tech Note
1957
25 pages
Report
English
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