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Experimental study of flow distribution for aviation kerosene in parallel helical tubes under supercritical pressure

https://doi.org/10.1016/j.applthermaleng.2015.06.082
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38/38 checkable references clean · checked 2026-07-23

Every reference with a DOI in the deposited reference list resolved to a known work in Crossref or DataCite at the dated check, and none carried a retraction, withdrawal, or removal notice.

7 without a DOI — not checked. A reference deposited without a DOI is never matched by title or guessed at; it stays outside the checked set, and this line discloses that.

The 38 checked references that resolve
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The 7 references without a DOI — listed, not checked
no DOI — not checkedCooled cooling air systems for turbine thermal management
no DOI — not checked10.1016/j.applthermaleng.2015.06.082_bib3
no DOI — not checkedEndothermic fuels for high mach vehicles
no DOI — not checkedD. Tompkins, T. Yoo, P. Hrnjak, T. Newell, K. Cho, International Refrigeration and Air Conditioning Conference at Purdue in 2002, R6-4, 554
no DOI — not checkedA numerical procedure for flow distribution and pressure drops for U and Z type configurations plate heat exchangers with variable coefficients
no DOI — not checkedEnthalpy measurement and heat transfer investigation of RP-3 kerosene at supercritical pressure
no DOI — not checkedFlow resistance characteristics of supercritical aviation kerosene in helix tube
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