Non-linear dynamic-motion characteristics of a series of missile configurations from simulated flight behaviour at mach numbers of 1.6 and 2.0

dc.contributor.author	I. M. Titchener	en_US
dc.date.accessioned	2014-10-21T15:51:00Z
dc.date.available	2014-10-21T15:51:00Z
dc.date.issued	1973	en_US
dc.identifier.other	ARC/R&M-3764	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3043
dc.description.abstract	Non-linear oscillatory-motion histories, measured in the R.A.E. wind-tunnel/flight-dynamics simulator, are analysed. The resulting dynamic-motion characteristics for large-amplitude motions in the pitch plane are discussed in relation to the aerodynamic features of the various configurations tested, and a simple dimensionless mathematical model is specified.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Non-linear dynamic-motion characteristics of a series of missile configurations from simulated flight behaviour at mach numbers of 1.6 and 2.0	en_US