2005
DOI: 10.21236/ada441027
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Aero-Elastic Motion of a Spin-Stabilized Projectile

Abstract: Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing the burden, to Department of Defense, Washington Headquarters Services, Directorate for Informat… Show more

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Cited by 1 publication
(1 citation statement)
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“…In the literature, several efforts have been well documented (Chae, 2004;Chae and Hodges, 2003;Haddadpour, 2006;Heddadj and Cayzac, 2000;Livshits et al, 1996;Meyers, 1973;Murphy and Mermagen, 2001;Murphy and Mermagen, 2005;Platus, 1992), regarding the investigation of the flight dynamic/aeroelastic response behavior of free flight spinning (or not) rockets and missiles. Moreover, in some studies the coupling between flight mechanics, aeroelasticity, and control system (aeroservoelastic coupling) has been investigated (Haddadpour, 2006).…”
Section: Introductionmentioning
confidence: 99%
“…In the literature, several efforts have been well documented (Chae, 2004;Chae and Hodges, 2003;Haddadpour, 2006;Heddadj and Cayzac, 2000;Livshits et al, 1996;Meyers, 1973;Murphy and Mermagen, 2001;Murphy and Mermagen, 2005;Platus, 1992), regarding the investigation of the flight dynamic/aeroelastic response behavior of free flight spinning (or not) rockets and missiles. Moreover, in some studies the coupling between flight mechanics, aeroelasticity, and control system (aeroservoelastic coupling) has been investigated (Haddadpour, 2006).…”
Section: Introductionmentioning
confidence: 99%