Structure Design and Heat Transfer Performance Analysis of a Novel Composite Phase Change Active Cooling Channel Wall for Hypersonic Aircraft.

Micromachines (Basel) · 2024 · PMC11123016 · PMID 38793196

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a decreasing trendno p-value reported

an increasing trendno p-value reported

The temperature exhibits a decreasing trend followed by an increasing trend, with the lowest temperature dropping by nearly 5 K compared to the highest temperature in the non-PCM region.

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