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Article

Development of RP-3 Surrogate Fuels via Multi-Objective Genetic Algorithm for Regenerative Cooling CFD with Supercritical Property Fidelity

1
Department of Aerospace and Mechanical Engineering, Korea Aerospace University, Goyang 10540, Republic of Korea
2
Department of Smart Air Mobility, Korea Aerospace University, Goyang 10540, Republic of Korea
3
School of Aerospace and Mechanical Engineering, Korea Aerospace University, Goyang 10540, Republic of Korea
*
Author to whom correspondence should be addressed.
Aerospace 2026, 13(4), 307; https://doi.org/10.3390/aerospace13040307
Submission received: 27 February 2026 / Revised: 20 March 2026 / Accepted: 24 March 2026 / Published: 25 March 2026
(This article belongs to the Section Astronautics & Space Science)

Abstract

Supercritical heat transfer in regenerative cooling channels is strongly influenced by thermophysical property variations near the pseudo-critical temperature, yet their direct implications for cooling performance have not been fully addressed. This study investigates how incorporating supercritical property considerations into surrogate fuel formulation affects heat transfer behavior in a regenerative cooling channel. RP-3 surrogate fuels were constructed using a genetic algorithm by matching both temperature-independent properties and temperature-dependent properties under supercritical conditions. Unlike previous approaches employing distillation curves as a secondary objective, the present formulation adopted supercritical density distribution and pseudo-critical temperature (Tpc) as optimization targets. The formulated surrogate fuels were evaluated in a regenerative cooling channel model surrounding a combustor, and their flow and heat transfer characteristics were compared with those of literature-based surrogate fuels. The results show that differences in Tpc and density variation trends significantly influence buoyancy-induced asymmetric flow structures and the onset of heat transfer deterioration. Surrogate fuels with lower Tpc exhibit earlier density reduction and earlier development of asymmetric flow, whereas fuels with higher Tpc demonstrate relatively mitigated wall temperature rise. The results of the present study suggest that surrogate fuel formulation based on supercritical thermophysical properties can have a significant influence on the predicted heat transfer behavior in regenerative cooling channels under the operating conditions considered.
Keywords: regenerative cooling channel; surrogate fuel; genetic algorithm; supercritical heat transfer; pseudo-critical temperature; heat transfer deterioration regenerative cooling channel; surrogate fuel; genetic algorithm; supercritical heat transfer; pseudo-critical temperature; heat transfer deterioration

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MDPI and ACS Style

Ko, S.; Gil, Y.; Park, S. Development of RP-3 Surrogate Fuels via Multi-Objective Genetic Algorithm for Regenerative Cooling CFD with Supercritical Property Fidelity. Aerospace 2026, 13, 307. https://doi.org/10.3390/aerospace13040307

AMA Style

Ko S, Gil Y, Park S. Development of RP-3 Surrogate Fuels via Multi-Objective Genetic Algorithm for Regenerative Cooling CFD with Supercritical Property Fidelity. Aerospace. 2026; 13(4):307. https://doi.org/10.3390/aerospace13040307

Chicago/Turabian Style

Ko, Sangho, Yuchang Gil, and Sungwoo Park. 2026. "Development of RP-3 Surrogate Fuels via Multi-Objective Genetic Algorithm for Regenerative Cooling CFD with Supercritical Property Fidelity" Aerospace 13, no. 4: 307. https://doi.org/10.3390/aerospace13040307

APA Style

Ko, S., Gil, Y., & Park, S. (2026). Development of RP-3 Surrogate Fuels via Multi-Objective Genetic Algorithm for Regenerative Cooling CFD with Supercritical Property Fidelity. Aerospace, 13(4), 307. https://doi.org/10.3390/aerospace13040307

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