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26006

NEW CONCEPTS IN THRUST AUGMENTOR EJECTORS

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Last updated: 04 Jan 2025

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Abstract

An investigation of both an experimental and theoretical nature has been conducted into the use of a subsonic conventional ejector as a thrust augmentor. A new effectiveness performance parameter, EN, was derived in this investigation and has proved a useful tool in comparing different thrust augmentor designs. Moderate ejector diffuser area ratios, around 1.5:1, were round to he more favourable for thrust augmentation. This dis(')very proves a new concept in ejector augmentor design which is more suitablc in airfield applications.

DOI

10.21608/asat.1987.26006

Authors

First Name

RAMADAN

Last Name

EL-BANNA

MiddleName

AHMED

Affiliation

Lecturer, Head of Aeronautical Department, Air Force Academy, Belbeis, Egypt

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Orcid

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Volume

2

Article Issue

A.S.A.T. CONFERENCE 21-23 April 1987 , CAIRO

Related Issue

4700

Issue Date

1987-04-01

Receive Date

2019-01-27

Publish Date

1987-04-01

Page Start

311

Page End

323

Print ISSN

2090-0678

Online ISSN

2636-364X

Article File

ASAT_Volume 2_Issue A.S.A.T. CONFERENCE 21-23 April 1987 , CAIRO_Pages 311-323.pdf

PDF . 1.9MB

Link

https://asat.journals.ekb.eg/article_26006.html

Detail API

https://asat.journals.ekb.eg/service?article_code=26006

Order

19

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

NEW CONCEPTS IN THRUST AUGMENTOR EJECTORS

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Article

Created At

22 Jan 2023