2010
DOI: 10.1007/s00419-010-0424-9
|View full text |Cite
|
Sign up to set email alerts
|

Analytical investigation of boundary layer growth and swirl intensity decay rate in a pipe

Abstract: In this research, the developing turbulent swirling flow in the entrance region of a pipe is investigated analytically by using the boundary layer integral method. The governing equations are integrated through the boundary layer and obtained differential equations are solved with forth-order Adams predictor-corrector method. The general tangential velocity is applied at the inlet region to consider both free and forced vortex velocity profiles. The comparison between present model and available experimental d… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
2

Citation Types

0
13
0

Year Published

2011
2011
2021
2021

Publication Types

Select...
5

Relationship

0
5

Authors

Journals

citations
Cited by 19 publications
(13 citation statements)
references
References 26 publications
0
13
0
Order By: Relevance
“…Then, the obtained differential equations are solved with the fourth-order Adams predictorcorrector method [27] . It must be mentioned that this study is the continuation of the previous study done by [26] on swirling flows.…”
Section: Fig 1 General Tangential Velocity Profilementioning
confidence: 93%
See 4 more Smart Citations
“…Then, the obtained differential equations are solved with the fourth-order Adams predictorcorrector method [27] . It must be mentioned that this study is the continuation of the previous study done by [26] on swirling flows.…”
Section: Fig 1 General Tangential Velocity Profilementioning
confidence: 93%
“…In most of the previous studies on the boundary layer such as [11] and [12], although a constant pressure gradient is considered due to the small thickness of the boundary layer, due to the high rotational velocity, the variation of the pressure inside the boundary layer has an important effect on the growth of the boundary layer [26] . To predict the pressure gradient, u θ inside the boundary layer is ignored.…”
Section: Solution Methodologymentioning
confidence: 99%
See 3 more Smart Citations