Show simple item record

contributor authorA. R. Kriebel
date accessioned2017-05-08T23:21:04Z
date available2017-05-08T23:21:04Z
date copyrightDecember, 1964
date issued1964
identifier issn0098-2202
identifier otherJFEGA4-27256#655_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/100335
description abstractThe internal structure of a normal shock wave in a perfect gas heavily laden with particles having a distribution of sizes is machine computed by numerical integration. The results of a small-perturbation analysis for weak shock waves and one particle size compare well with the machine-computed results for these restricted conditions. Both methods indicate that the thickness of weak shock waves increases in proportion to the particle size squared and inversely with the shock strength. For conditions typical of solid propellant-rocket motor exhaust streams the computed shock-wave thickness is several inches. With such computed results both the amount and the size distribution of suspended particles can be found individually from shock-wave measurements.
publisherThe American Society of Mechanical Engineers (ASME)
titleAnalysis of Normal Shock Waves in Particle Laden Gas
typeJournal Paper
journal volume86
journal issue4
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3655914
journal fristpage655
journal lastpage664
identifier eissn1528-901X
keywordsParticulate matter
keywordsShock waves
keywordsParticle size
keywordsMachinery
keywordsThickness
keywordsMeasurement
keywordsEngines
keywordsPropellants
keywordsRockets
keywordsShock (Mechanics) AND Exhaust systems
treeJournal of Fluids Engineering:;1964:;volume( 086 ):;issue: 004
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record