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Development of a wind retrieval method for low-speed low-pressure flows for ExoMars
Luleå University of Technology, Department of Computer Science, Electrical and Space Engineering, Space Technology.ORCID iD: 0000-0002-8768-2539
Luleå University of Technology, Department of Computer Science, Electrical and Space Engineering, Space Technology. Centro de Astrobiología (INTA-CSIC), Torrejón de Ardoz, 28850 Madrid, Spain.ORCID iD: 0000-0002-4492-9650
Luleå University of Technology, Department of Computer Science, Electrical and Space Engineering, Space Technology.ORCID iD: 0000-0002-4474-9983
Luleå University of Technology, Department of Computer Science, Electrical and Space Engineering, Space Technology. Instituto Andaluz de Ciencias de la Tierra (CSIC-UGR), 18100 Granada, Spain.ORCID iD: 0000-0001-6479-2236
2020 (English)In: Applied Thermal Engineering, ISSN 1359-4311, E-ISSN 1873-5606, Vol. 180, article id 115752Article in journal (Refereed) Published
Abstract [en]

Forced convective heat transfer from three horizontally inclined rectangular-based cylinders (rods) has been studied experimentally under representative Martian near-surface air flows in the Aarhus Wind Tunnel Simulator (AWTS), Denmark. The testing campaign was developed for the HABIT (Habitability: Brines, Irradiation and Temperature) instrument, European payload on board the ExoMars 2022 Kazachok surface platform. The average heat transfer coefficient was determined from steady CO2 flows at a pressure of 9.9 mbar, an ambient temperature of ∼25 °C, and for horizontal free-stream velocities between 0.8 and 12 m/s. A retrieval algorithm to derive the wind speed from the average heat transfer coefficient estimated at each of the three HABIT Air Temperature Sensors (ATS) rods was calibrated within the AWTS. The ATS rods are placed one at the front of the instrument structure (ATS2) and two on the sides (ATS1 and ATS3); and under Martian atmospheric conditions these rods serve as cooling fins. Several relationships between the Nusselt number and the Reynolds and Prandtl numbers reported in the literature were evaluated to model convective heat transfer from the ATS rods. Where needed, corrections to account for radiative heat transfer within the AWTS were implemented. The final retrieval method demonstrated that wind speed can be retrieved for frontal winds in the range of 0–10 m/s, with an error of ±0.3 m/s, using the cooling profile of the ATS rod 3, and for lateral winds in the range of 0–6 m/s, with an error of ±0.3 m/s, using the ATS rod 2 cooling profile.

Place, publisher, year, edition, pages
Elsevier, 2020. Vol. 180, article id 115752
Keywords [en]
Heat transfer coefficient, Forced convection, Wind tunnel, Nusselt number, Experiments, Mars
National Category
Aerospace Engineering
Research subject
Atmospheric science
Identifiers
URN: urn:nbn:se:ltu:diva-80534DOI: 10.1016/j.applthermaleng.2020.115752ISI: 000569818200014Scopus ID: 2-s2.0-85088962817OAI: oai:DiVA.org:ltu-80534DiVA, id: diva2:1460532
Note

Validerad;2020;Nivå 2;2020-08-24 (alebob)

Available from: 2020-08-24 Created: 2020-08-24 Last updated: 2021-12-13Bibliographically approved

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Soria-Salinas, ÁlvaroZorzano, María-PazMantas-Nakhai, RobertoMartín-Torres, Javier

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