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Thermal compensation in recessed piezoresistive probes to improve absolute pressure measurements in rotating detonation engines

Published Online: 2025-08-06

Published Print: 2025-08

Authors

Miller, Robert S.

Agrawal, Ajay K.

Hilton, John P.
License Information

Text and Data Mining valid from 2025-08-01

Version of Record valid from 2025-08-01
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Article History

Received: 30 March 2025

Revised: 13 July 2025

Accepted: 14 July 2025

First Online: 6 August 2025

Declarations

:

: The authors declare no competing interests.

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