Beta
ManageSearchChatDiscover
26465

ALGEBRAIC PREDICTION OF TURBULENT BOUNDARY LAYERS IN ADVERSE PRESSURE GRADIENT

Article

Last updated: 04 Jan 2025

OverviewSimilar Items

Subjects

-

Tags

-

Abstract

An attempt has been made to develop a method for predicting the development of turbulent boundary layers in adverse pressure gradient. Simple calculation procedure is presented by incorp-orating a deceleration rate parameter into boundary layer equations. The compressibility effect of the flow is considered° by adopting the Mach number in the momentum and skin friction relations. The predictions of the boundary layers are in good agreement with available experimental results,which validates the calculational technique.

DOI

10.21608/asat.1985.26465

Authors

First Name

A.

Last Name

EL-KERSH

MiddleName

M.

Affiliation

Lecturer,Mechanical Engineering Dept.,Faculty of Engineering and Technology,Minia University,Minia,Egypt.

Email

-

City

-

Orcid

-

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

2019-02-04

Publish Date

1985-05-01

Page Start

39

Page End

60

Print ISSN

2090-0678

Online ISSN

2636-364X

Article File

ASAT_Volume 1_Issue A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO_Pages 39-60.pdf

PDF . 3.4MB

Link

https://asat.journals.ekb.eg/article_26465.html

Detail API

https://asat.journals.ekb.eg/service?article_code=26465

Order

5

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

ALGEBRAIC PREDICTION OF TURBULENT BOUNDARY LAYERS IN ADVERSE PRESSURE GRADIENT

Details

Type

Article

Created At

22 Jan 2023