Beta
ManageSearchChatDiscover
24418

A Preliminary Design for Multistage Axial Flow Compressors Part 11: Case study

Article

Last updated: 04 Jan 2025

OverviewSimilar Items

Subjects

-

Tags

-

Abstract

The computer package developed for the preliminary design of multistage axial compressor described in part (I) is applied here for the design of compressor of a typical aeroengine.This compressor is in close proximity to compressor in the CF6-60 turbofan engine. For the same design conditions, the calculated compressor has the same number of stages and layout as that of the CF6 engine. Detailed results concerning both aerodynamic and mechanical designs are presented here.

DOI

10.21608/asat.2013.24418

Keywords

Multistage Axial Compressor, Two Dimensional, hub-to-tip variation, Blade geometry, CF6 turbofan

Authors

First Name

Ahmed

Last Name

Abdel Azim

MiddleName

F.

Affiliation

Professor and head, Mechanical Power Engineering Dept, Zagazig University.

Email

-

City

-

Orcid

-

First Name

Ahmed

Last Name

Hamed

MiddleName

-

Affiliation

Research engineer, Egypt Air co.

Email

-

City

-

Orcid

-

First Name

Wael

Last Name

Shehata

MiddleName

-

Affiliation

Research engineer, Egypt Air co.

Email

-

City

-

Orcid

-

Volume

10

Article Issue

10th International Conference On Aerospace Sciences & Aviation Technology

Related Issue

4497

Issue Date

2003-05-01

Receive Date

2019-01-14

Publish Date

2003-05-01

Page Start

169

Page End

184

Print ISSN

2090-0678

Online ISSN

2636-364X

Article File

ASAT_Volume 10_Issue 10th International Conference On Aerospace Sciences & A….pdf

PDF . 2.4MB

Link

https://asat.journals.ekb.eg/article_24418.html

Detail API

https://asat.journals.ekb.eg/service?article_code=24418

Order

12

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

A Preliminary Design for Multistage Axial Flow Compressors Part 11: Case study

Details

Type

Article

Created At

22 Jan 2023