2017
DOI: 10.1016/j.ijheatmasstransfer.2016.10.119
|View full text |Cite
|
Sign up to set email alerts
|

Heat transfer and pressure loss in swirl tubes with one and multiple tangential jets pertinent to gas turbine internal cooling

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1
1

Citation Types

1
8
0

Year Published

2019
2019
2024
2024

Publication Types

Select...
7

Relationship

0
7

Authors

Journals

citations
Cited by 51 publications
(9 citation statements)
references
References 18 publications
1
8
0
Order By: Relevance
“…The average Nusselt numbers for the four turbulence models are presented in difference. This latter figure is close to the results of [35], where the difference between SST predicted values and measured values of average Nusselt numbers ranged between 8% and 13%. The RNG kε model was adopted for all the following calculations, not only because of its ability to predict the heat transfer and velocity profiles more accurately, but also its low computational cost.…”
Section: Validationsupporting
confidence: 89%
“…The average Nusselt numbers for the four turbulence models are presented in difference. This latter figure is close to the results of [35], where the difference between SST predicted values and measured values of average Nusselt numbers ranged between 8% and 13%. The RNG kε model was adopted for all the following calculations, not only because of its ability to predict the heat transfer and velocity profiles more accurately, but also its low computational cost.…”
Section: Validationsupporting
confidence: 89%
“…And they also explained the flow and heat transfer characteristics of swirl tubes with single tangential jets are significantly different from those with multi-tangential jets. The swirl heat transfer tube with multiple tangential jets shows more practical performance and can achieve stronger and more uniform heat transfer distribution [25]. In addition, Liu et al [26], Biegger et al [24], and Bruschewski et al [27] have conducted numerical simulations of swirling flow in a tube using RANS (Reynolds averaged numerical simulation), DES (detached eddy simulation), and LES (large eddy simulation) and obtained flow field results that matched the experimental heat transfer results.…”
Section: Introductionmentioning
confidence: 86%
“…Figure 2 provides a schematic of the computational geometry of anti-icing inner fluid, where the circular tube has a length of 1000 mm and a diameter of 50 mm, conforming precisely to the specifications outlined in Ref. [25]. The hot air is extracted from engine compressor and passes through five holes to reach the inner anti-icing surface, and the five holes are of three types, which are the impingement jets, offset jets, and swirl jets.…”
Section: Numerical Setupsmentioning
confidence: 99%
“…Experimental work on the behavior of a shell‐tube exchanger was performed by Ghorbani et al 19 It was shown that flow rate was the main factor in temperature behavior along the system. Rao et al 20 investigated experimentally the effect of single and double tangential jets relevant to gas turbine internal cooling and pressure loss. Findings showed that two different inlet jet modes possess different heat transfer patterns.…”
Section: Introductionmentioning
confidence: 99%