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25944

MATHEMATICAL MODELING OF THE AIR PRESSURE REDUCER OPTIMUM NOZZLE DIAMETER OF ITS TESTING PIPE

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Last updated: 04 Jan 2025

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Abstract

One of the most important elements in the pneumatic circuits is the pressure reducer which is commonly used to keep a constant downstream pressure, whatever the value of the upstream one. In fact the downstream pressure would anyway vary, but it could be considered to operate with a sufficient accuracy if its outlet. pressure varies within a zone of ±5% of its nominal value. That is why every pressure reducer, after being manufactured then assembled; must be tested to verify its function, and whether it works in the prescribed tolerance. The testing bench consists of several pressurized air bottles, branches to the pressure reducer, downstream of which there mounted a short pipe of inner diameter: dpipe ; nozzled at its outlet end witha diameter: dn. In the present research, a complete mathematical model is developed to find out the optimum nozzle diameter of the testing section which is necessary to identify the function of certain reducer.

DOI

10.21608/asat.1989.25944

Authors

First Name

A.

Last Name

KHATTAB

MiddleName

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Affiliation

Dr., Assistant Prof., Dept. of mech. power & energy, MfC,CAIRO, EGYPT.

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First Name

G.

Last Name

RABIE

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Affiliation

Dr., Associate Prof., Dept. of aircraft, MTC, CAIRO, EGYPT.

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Orcid

-

First Name

O.

Last Name

GAWEISH

MiddleName

-

Affiliation

Eng., Arab British Dynamics (ABD), System engineering dept,, Cairo, EGYPT.

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Orcid

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First Name

S.

Last Name

ZAHRAN

MiddleName

-

Affiliation

Dr., Assistant Prof., Mech. Dept. ,Faculty of engineering at SHOBRA, CAIRO, EGYPT.

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-

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Volume

3

Article Issue

ASAT Conference 4-6 April 1989 , CAIRO

Related Issue

4687

Issue Date

1989-04-01

Receive Date

2019-01-27

Publish Date

1989-04-01

Page Start

383

Page End

396

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_25944.html

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https://asat.journals.ekb.eg/service?article_code=25944

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21

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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

MATHEMATICAL MODELING OF THE AIR PRESSURE REDUCER OPTIMUM NOZZLE DIAMETER OF ITS TESTING PIPE

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Article

Created At

22 Jan 2023