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This is a Experimental Study study.

September 19, 2025Proceedings

Experimentally-resolved flow and thermal fields at the Exit of an annular non-reacting combustor sector

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Experiments show swirling flow alters thermal fields in a non-reacting combustor, indicating variations impact pressure gradients.

Different swirlers significantly changed the pressure and velocity fields at the combustor exit.
A seven-hole probe with a thermocouple was used to resolve flow and thermal fields for various swirling flow intensities.
The mixing intensity between mainstream and cooling air was affected by changes in swirler configuration.
The temperature ratio of hot mainstream to cooling air minimally influenced flow behaviors yet affected pressure gradients.

Li et al. (2025) studied this question.

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September 19, 2025Proceedings

View Full Paper

Ask AI

Bookmark

Authors

Experiments show swirling flow alters thermal fields in a non-reacting combustor, indicating variations impact pressure gradients.

Different swirlers significantly changed the pressure and velocity fields at the combustor exit.
A seven-hole probe with a thermocouple was used to resolve flow and thermal fields for various swirling flow intensities.
The mixing intensity between mainstream and cooling air was affected by changes in swirler configuration.
The temperature ratio of hot mainstream to cooling air minimally influenced flow behaviors yet affected pressure gradients.

Li et al. (2025) studied this question.

View Full Paper

Ask AI

Bookmark