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26512

THE PARTICLE-IN-CELL MODEL FOR GAS-DROPLET FLOWS IN SHOCK-TUBES

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Last updated: 04 Jan 2025

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Abstract

The present work investigates the propagation of incident and reflected shock and rarefaction waves in a homogeneous mixture of gas and liquid droplets in shock-tubes. Two models describing the break-up process of drops exposed to blasts of air were used. The governing enuations were solved using the Particle-In-Cell (pic) method, and was developed specif-ically to be run on a micro-computer, and to overcome the disadvantages of relatively low speed and limited memory resources of micro-computers compared to main frames. The numerical solution remains stable for low and moderate droplet volume fractions and the predicted velocity,pressure and temperature flow fields for the gas and droplet phases aptly illustrate the capability of the method to treat the complex coupling phenomena associated with multi-phase flows and shows its dependence on the physical properties of both gas and droplets.

DOI

10.21608/asat.1985.26512

Authors

First Name

ASSEM.

Last Name

Z.

MiddleName

M.

Affiliation

Mech. Engg. Dept., Air Defence Colg., Alex., EGYPT.

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Orcid

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First Name

WARDA.

Last Name

A.

MiddleName

H.

Affiliation

Mech. Engg. Dept., Alexandria Univ., Alex., EGYPT.

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Volume

1

Article Issue

A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO

Related Issue

4758

Issue Date

1985-05-01

Receive Date

2019-02-05

Publish Date

1985-05-01

Page Start

329

Page End

339

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_26512.html

Detail API

https://asat.journals.ekb.eg/service?article_code=26512

Order

26

Type

Original Article

Type Code

737

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

https://asat.journals.ekb.eg/

MainTitle

THE PARTICLE-IN-CELL MODEL FOR GAS-DROPLET FLOWS IN SHOCK-TUBES

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Article

Created At

22 Jan 2023