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Experimental investigation of heating augmentation by particle kinetic energy conversion in dust laden supersonic flows

Allofs, Dirk und Neeb, Dominik und Gülhan, Ali (2023) Experimental investigation of heating augmentation by particle kinetic energy conversion in dust laden supersonic flows. Experiments in Fluids, 64. Springer Nature. doi: 10.1007/s00348-023-03718-4. ISSN 0723-4864.

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Offizielle URL: https://link.springer.com/content/pdf/10.1007/s00348-023-03718-4.pdf

Kurzfassung

The presence of particles in supersonic flows can cause significant increases in stagnation point heat fluxes (Dunbar et al. in AIAA J 13:908–912, 1975). This effect is commonly named particle-induced heat flux augmentation or just heating augmentation. Heating augmentation can be described as the sum of the conversion of kinetic energy of the particles into thermal energy, characterized by the energy conversion efficiency, also called accommodation coefficient, and the increase of convective heat flux (Polezhaev et al. in High Temp 30:1147–1153, 1992; Vasilevskii and Osiptsov in Experimental and numerical study of heat transfer on a blunt body in dusty hypersonic flow 33rd thermophysics conference, American Institute of Aeronautics and Astronautics, 1999). Although the accommodation coefficient is fundamental for heating augmenta- tion characterization, there is only a small number of experimental datasets for it. This work focusses on the experimental determination of the accommodation coefficient in flow regimes at Mach number 2.1, Reynolds number, based on the probe nose diameter, from approx. 6e5 to 1.8e6, and nominal particle sizes of approx. 20 um. The decrease of particle velocity and kinetic energy flux in the shock layer is measured with highly resolved shadowgraphy for individual particles. The particle kinetic energy flux is decreased by 29% on average by particle deceleration in the shock layer. Negligible kinetic energy fluxes of rebounded particles were measured. The accommodation coefficient is approx. 0.36 for Al 2 O 3 and SiO 2 particles, while it is approx. 0.09 for MgO particles. Hence, it is significantly smaller than the widely used value of 0.7, based on the study of (Fleener and Watson in Convective heating in dust-laden hypersonic flows 8th thermophysics conference, 1973), but in good agreement with values given in (Hove and Shih in Reentry vehicle stagnation region heat transfer in particle environments 15th aerospace sciences meeting, 1977) and (Molleson and Stasenko in High Temp 55:87–94, 2017. https:// doi.org/10.1134/S0018151X1701014X ). No difference between erosive and elastic particle reflection mode was detected on the conversion efficiency. The data from a simplification of the modeling approach of the conversion efficiency for elastic particle reflection by Molleson and Stasenko (2017) are in poor agreement with experimental data.

elib-URL des Eintrags:https://elib.dlr.de/200841/
Dokumentart:Zeitschriftenbeitrag
Titel:Experimental investigation of heating augmentation by particle kinetic energy conversion in dust laden supersonic flows
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Allofs, DirkDirk.Allofs (at) dlr.dehttps://orcid.org/0000-0002-3776-1853NICHT SPEZIFIZIERT
Neeb, DominikDominik.Neeb (at) dlr.dehttps://orcid.org/0000-0002-5848-3055NICHT SPEZIFIZIERT
Gülhan, AliAli.Guelhan (at) dlr.dehttps://orcid.org/0000-0003-4905-5881NICHT SPEZIFIZIERT
Datum:30 Oktober 2023
Erschienen in:Experiments in Fluids
Referierte Publikation:Ja
Open Access:Ja
Gold Open Access:Nein
In SCOPUS:Ja
In ISI Web of Science:Ja
Band:64
DOI:10.1007/s00348-023-03718-4
Verlag:Springer Nature
ISSN:0723-4864
Status:veröffentlicht
Stichwörter:Particle Size, Velocity, number concentration, two phase flows, dust-laden flows, supersonic flows, shock layer, particle kinetic energy, heat flux augmentation, heating augmentation, stagnation point heat flux, convective heat flux, accomodation coefficient
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Raumfahrt
HGF - Programmthema:Raumtransport
DLR - Schwerpunkt:Raumfahrt
DLR - Forschungsgebiet:R RP - Raumtransport
DLR - Teilgebiet (Projekt, Vorhaben):R - XTRAS - EXperTiese RAumtranSport
Standort: Köln-Porz
Institute & Einrichtungen:Institut für Aerodynamik und Strömungstechnik > Über- und Hyperschalltechnologien, KP
Hinterlegt von: Allofs, Dirk
Hinterlegt am:14 Dez 2023 09:29
Letzte Änderung:14 Dez 2023 09:29

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