Analysis of Normal Shock Waves in Particle Laden GasSource: Journal of Fluids Engineering:;1964:;volume( 086 ):;issue: 004::page 655Author:A. R. Kriebel
DOI: 10.1115/1.3655914Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The 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.
keyword(s): Particulate matter , Shock waves , Particle size , Machinery , Thickness , Measurement , Engines , Propellants , Rockets , Shock (Mechanics) AND Exhaust systems ,
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contributor author | A. R. Kriebel | |
date accessioned | 2017-05-08T23:21:04Z | |
date available | 2017-05-08T23:21:04Z | |
date copyright | December, 1964 | |
date issued | 1964 | |
identifier issn | 0098-2202 | |
identifier other | JFEGA4-27256#655_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/100335 | |
description abstract | The 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. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Analysis of Normal Shock Waves in Particle Laden Gas | |
type | Journal Paper | |
journal volume | 86 | |
journal issue | 4 | |
journal title | Journal of Fluids Engineering | |
identifier doi | 10.1115/1.3655914 | |
journal fristpage | 655 | |
journal lastpage | 664 | |
identifier eissn | 1528-901X | |
keywords | Particulate matter | |
keywords | Shock waves | |
keywords | Particle size | |
keywords | Machinery | |
keywords | Thickness | |
keywords | Measurement | |
keywords | Engines | |
keywords | Propellants | |
keywords | Rockets | |
keywords | Shock (Mechanics) AND Exhaust systems | |
tree | Journal of Fluids Engineering:;1964:;volume( 086 ):;issue: 004 | |
contenttype | Fulltext |