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contributor authorW. S. Hart
date accessioned2017-05-09T01:34:38Z
date available2017-05-09T01:34:38Z
date copyrightMarch, 1972
date issued1972
identifier issn0098-2202
identifier otherJFEGA4-27389#53_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/162889
description abstractMotion pictures of launches of Titan III solid rocket motors were used, in conjunction with conservation equations and knowledge of rocket plume properties, to determine the initial temperature and mass of the large cloud that is generated during these launches. These initial conditions were applied to a mathematical model which accounted for buoyancy, drag and entrainment. The model predicted the radius, altitude, temperature and mass of the cloud as a function of time. The results showed fair agreement with size and altitude data extracted from the movies. This methodology was applied with limited success to smaller scale rocket clouds generated at test stands. The model was also used to predict the behavior of large exhaust clouds under various external temperature profiles. There is some experimental evidence that the model correctly accounts for unstable profiles, and the predictions of cloud rise during inversion conditions agree with what intuition would predict.
publisherThe American Society of Mechanical Engineers (ASME)
titleDynamics of Large Buoyant Clouds Generated by Rocket Launches
typeJournal Paper
journal volume94
journal issue1
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3425385
journal fristpage53
journal lastpage60
identifier eissn1528-901X
keywordsDynamics (Mechanics)
keywordsRockets
keywordsTemperature
keywordsMotion
keywordsMotors
keywordsDrag (Fluid dynamics)
keywordsPlumes (Fluid dynamics)
keywordsEquations
keywordsExhaust systems
keywordsTemperature profiles AND Buoyancy
treeJournal of Fluids Engineering:;1972:;volume( 094 ):;issue: 001
contenttypeFulltext


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