Show simple item record

contributor authorFidelis O. Eke
contributor authorTai-Chien Mao
contributor authorMichael J. Morris
date accessioned2017-05-09T00:12:08Z
date available2017-05-09T00:12:08Z
date copyrightMarch, 2004
date issued2004
identifier issn0021-8936
identifier otherJAMCAV-26575#190_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/129510
description abstractThis paper explores the various analytical links between the free attitude motions of spinning bodies of the rocket type, and the system’s parameters. The system is modeled as an axisymmetric body with substantial mass loss, and special attention is paid to the presence of a nozzle on the system. It is found that the nozzle expansion ratio can have an important influence on attitude motion, the higher this ratio the better behaved the system.
publisherThe American Society of Mechanical Engineers (ASME)
titleFree Attitude Motions of a Spinning Body With Substantial Mass Loss
typeJournal Paper
journal volume71
journal issue2
journal titleJournal of Applied Mechanics
identifier doi10.1115/1.1653738
journal fristpage190
journal lastpage194
identifier eissn1528-9036
keywordsNozzles
keywordsEquations
keywordsPropellants
keywordsRockets
keywordsRotating bodies
keywordsMotion
keywordsParticle spin AND Shapes
treeJournal of Applied Mechanics:;2004:;volume( 071 ):;issue: 002
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record