Experimental Investigation on Heat Transfer Mechanism of Air-Blast-Spray-Cooling System with a Two-Phase Ejector Loop for Aeronautical Application

This paper presents an air-oriented spray cooling system (SCS) integrated with a two-phase ejector for the thermal management system. Considering its aeronautical application, the spray nozzle in the SCS is an air-blast one. Heat transfer performance (HTP) of air-water spray cooling was studied expe...

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Main Authors: Jia-Xin Li, Yun-Ze Li, Ben-Yuan Cai, En-Hui Li
Format: Article
Language:English
Published: MDPI AG 2019-10-01
Series:Energies
Subjects:
Online Access:https://www.mdpi.com/1996-1073/12/20/3963
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spelling doaj-1c956146cc2a4b1fb8d8b458632c229b2020-11-25T02:42:44ZengMDPI AGEnergies1996-10732019-10-011220396310.3390/en12203963en12203963Experimental Investigation on Heat Transfer Mechanism of Air-Blast-Spray-Cooling System with a Two-Phase Ejector Loop for Aeronautical ApplicationJia-Xin Li0Yun-Ze Li1Ben-Yuan Cai2En-Hui Li3School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, ChinaSchool of Aeronautic Science and Engineering, Beihang University, Beijing 100191, ChinaSchool of Aeronautic Science and Engineering, Beihang University, Beijing 100191, ChinaSchool of Aeronautic Science and Engineering, Beihang University, Beijing 100191, ChinaThis paper presents an air-oriented spray cooling system (SCS) integrated with a two-phase ejector for the thermal management system. Considering its aeronautical application, the spray nozzle in the SCS is an air-blast one. Heat transfer performance (HTP) of air-water spray cooling was studied experimentally on the basis of the ground-based test. Factors including pressure difference between water-inlet-pressure (WIP) and spray cavity one (PDWIC) and the spray volumetric flow rate (SVFR) were investigated and discussed. Under a constant operating condition, the cooling capacity can be promoted by the growth factors of the PDWIC and SVFR with the values from 51.90 kPa to 235.35 kPa and 3.91 <inline-formula> <math display="inline"> <semantics> <mrow> <mi mathvariant="normal">L</mi> <mo>&#8901;</mo> <msup> <mi mathvariant="normal">h</mi> <mrow> <mrow> <mo>&#8722;</mo> <mn>1</mn> </mrow> </mrow> </msup> </mrow> </semantics> </math> </inline-formula> to 14.53 <inline-formula> <math display="inline"> <semantics> <mrow> <mi mathvariant="normal">L</mi> <mo>&#8901;</mo> <msup> <mi mathvariant="normal">h</mi> <mrow> <mrow> <mo>&#8722;</mo> <mn>1</mn> </mrow> </mrow> </msup> </mrow> </semantics> </math> </inline-formula>, respectively. Under the same heating power, HTP is proportional to the two dimensionless parameters Reynolds number and Weber number due to the growth of droplet-impacting velocity and droplet size as the increasing of PDWIC or SVFR. Additionally, compared with the factor of the droplet size, the HTP is more sensitive to the variation in the droplet-impacting velocity. Based on the experimental data, an empirical experimental correlation for the prediction of the dimensionless parameter Nusselt number in the non-boiling region with the relative error of only <inline-formula> <math display="inline"> <semantics> <mrow> <mo>&#177;</mo> <mn>10</mn> <mo>%</mo> </mrow> </semantics> </math> </inline-formula> was obtained based on the least square method.https://www.mdpi.com/1996-1073/12/20/3963spray coolingground-based test setuptwo-phase ejectoraeronautical applicationempirical experimental correlation
collection DOAJ
language English
format Article
sources DOAJ
author Jia-Xin Li
Yun-Ze Li
Ben-Yuan Cai
En-Hui Li
spellingShingle Jia-Xin Li
Yun-Ze Li
Ben-Yuan Cai
En-Hui Li
Experimental Investigation on Heat Transfer Mechanism of Air-Blast-Spray-Cooling System with a Two-Phase Ejector Loop for Aeronautical Application
Energies
spray cooling
ground-based test setup
two-phase ejector
aeronautical application
empirical experimental correlation
author_facet Jia-Xin Li
Yun-Ze Li
Ben-Yuan Cai
En-Hui Li
author_sort Jia-Xin Li
title Experimental Investigation on Heat Transfer Mechanism of Air-Blast-Spray-Cooling System with a Two-Phase Ejector Loop for Aeronautical Application
title_short Experimental Investigation on Heat Transfer Mechanism of Air-Blast-Spray-Cooling System with a Two-Phase Ejector Loop for Aeronautical Application
title_full Experimental Investigation on Heat Transfer Mechanism of Air-Blast-Spray-Cooling System with a Two-Phase Ejector Loop for Aeronautical Application
title_fullStr Experimental Investigation on Heat Transfer Mechanism of Air-Blast-Spray-Cooling System with a Two-Phase Ejector Loop for Aeronautical Application
title_full_unstemmed Experimental Investigation on Heat Transfer Mechanism of Air-Blast-Spray-Cooling System with a Two-Phase Ejector Loop for Aeronautical Application
title_sort experimental investigation on heat transfer mechanism of air-blast-spray-cooling system with a two-phase ejector loop for aeronautical application
publisher MDPI AG
series Energies
issn 1996-1073
publishDate 2019-10-01
description This paper presents an air-oriented spray cooling system (SCS) integrated with a two-phase ejector for the thermal management system. Considering its aeronautical application, the spray nozzle in the SCS is an air-blast one. Heat transfer performance (HTP) of air-water spray cooling was studied experimentally on the basis of the ground-based test. Factors including pressure difference between water-inlet-pressure (WIP) and spray cavity one (PDWIC) and the spray volumetric flow rate (SVFR) were investigated and discussed. Under a constant operating condition, the cooling capacity can be promoted by the growth factors of the PDWIC and SVFR with the values from 51.90 kPa to 235.35 kPa and 3.91 <inline-formula> <math display="inline"> <semantics> <mrow> <mi mathvariant="normal">L</mi> <mo>&#8901;</mo> <msup> <mi mathvariant="normal">h</mi> <mrow> <mrow> <mo>&#8722;</mo> <mn>1</mn> </mrow> </mrow> </msup> </mrow> </semantics> </math> </inline-formula> to 14.53 <inline-formula> <math display="inline"> <semantics> <mrow> <mi mathvariant="normal">L</mi> <mo>&#8901;</mo> <msup> <mi mathvariant="normal">h</mi> <mrow> <mrow> <mo>&#8722;</mo> <mn>1</mn> </mrow> </mrow> </msup> </mrow> </semantics> </math> </inline-formula>, respectively. Under the same heating power, HTP is proportional to the two dimensionless parameters Reynolds number and Weber number due to the growth of droplet-impacting velocity and droplet size as the increasing of PDWIC or SVFR. Additionally, compared with the factor of the droplet size, the HTP is more sensitive to the variation in the droplet-impacting velocity. Based on the experimental data, an empirical experimental correlation for the prediction of the dimensionless parameter Nusselt number in the non-boiling region with the relative error of only <inline-formula> <math display="inline"> <semantics> <mrow> <mo>&#177;</mo> <mn>10</mn> <mo>%</mo> </mrow> </semantics> </math> </inline-formula> was obtained based on the least square method.
topic spray cooling
ground-based test setup
two-phase ejector
aeronautical application
empirical experimental correlation
url https://www.mdpi.com/1996-1073/12/20/3963
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