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Thermal and Aerodynamic Characterization of a Creviced and Squared Piston Rapid Compression Machine: Extending the Validity of the Adiabatic Core Hypothesis, Generating Controlled Temperature Gradients

Crossref DOI link: https://doi.org/10.1007/s10494-023-00465-8

Published Online: 2023-08-19

Published Print: 2023-11

Update policy: https://doi.org/10.1007/springer_crossmark_policy

Authors

Ossman, H.

Strozzi, C.

Sotton, J.

Bellenoue, M.
Funding

Funding for this research was provided by:

CPER FEDER (P-2020-BAFE-38 - Transport_NEXTPROP, P-2019-BAFE-33 - COMBUMI)

French government program “Investissements d’Avenir” (EUR INTREE, reference ANR-18-EURE-0010)

Ministère de l'Education Nationale, de l'Enseignement Supérieur et de la Recherche
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Text and Data Mining valid from 2023-08-19

Version of Record valid from 2023-08-19
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Article History

Received: 21 April 2023

Accepted: 21 July 2023

First Online: 19 August 2023

Declarations

:

: The author declare that they have no conflict interest.

: This declaration is not applicable.

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