Superiority of Secondary Bypass Air in an Integrated Thermal Management System: A Multi-Level Simulation Study

Jie WEN , Mengchen LI , Guoqiang XU , Bensi DONG , Zhiwei LIU , Lei CHEN , Laihe ZHUANG

Engineering ›› : 202603017

PDF (3516KB)
Engineering ›› :202603017 DOI: 10.1016/j.eng.2026.03.017
research-article
Superiority of Secondary Bypass Air in an Integrated Thermal Management System: A Multi-Level Simulation Study
Author information +
History +
PDF (3516KB)

Abstract

With the advancement of next-generation fighter aircraft, the escalating cooling demands of thermal management in aircraft and their engines are approaching the thresholds of conventional heat sinks, including ram air and fuel. A variable cycle engine (VCE), characterized by its third-stream design, facilitates potential multi-heat sink coordination within the fuel thermal management system (FTMS). Despite the use of decoupled VCE and FTMS modeling in previous research, the heat sink potential of internal secondary bypass air remains largely unexplored and unquantified, with its feedback effects on VCE energy efficiency also lacking rigorous investigation. Driven by the background, this study proposes a novel coupling of VCE and FTMS design. By leveraging multidisciplinary simulations, we provide the first quantitative analysis of the heat sink efficacy of secondary bypass air across representative flight missions and elucidate its synergistic mechanism with fuel. Investigations reveal that compared with ram air, secondary bypass air markedly reduces the thermal accumulation by 36.57%–74.06%. This improved thermal performance is accompanied by a 2.17%–4.10% decrease in the hot-return fuel flow. Intriguingly, the induced specific fuel consumption penalty throughout various typical flight missions consistently remains below 0.8%, thereby demonstrating the economic efficiency and sustainable benefits of employing secondary bypass air for thermal management. Furthermore, this study presents the first optimization strategy for allocating heat transfer areas. Specifically, an area ratio of 0.6 between the ram air and secondary bypass air significantly lowers the system hot-return fuel temperature by 2.68%. This work validates quantitative evidence for secondary bypass air–FTMS coupling and establishes a foundation for system-level thermal management schemes in advanced fighter aircraft and engine designs.

Keywords

Fuel thermal management system / Variable cycle engine / Secondary bypass air / Coupling mechanism / Multi-level analysis

Cite this article

Download citation ▾
Jie WEN, Mengchen LI, Guoqiang XU, Bensi DONG, Zhiwei LIU, Lei CHEN, Laihe ZHUANG. Superiority of Secondary Bypass Air in an Integrated Thermal Management System: A Multi-Level Simulation Study. Engineering 202603017 DOI:10.1016/j.eng.2026.03.017

登录浏览全文

4963

注册一个新账户 忘记密码

References

[1]

Wang B , Zhao H , Yu L , Ye Z . Study of temperature effect on servovalve—controlled fuel metering unit. J Eng Gas Turbine Power 2015; 137(6):061503.

[2]

Fan H , Piao Y . Cooling design of an aero—engine fuel centrifugal pump at shut—off. Adv Mech Eng 2017; 9(6):1687814017709700.

[3]

Ebrahimi A , Jafari S , Nikolaidis T . Heat load development and heat map sensitivity analysis for civil aero—engines. Int J Turbomach Propuls Power 2024; 9(3):25.

[4]

Aygun H , Cilgin ME , Ekmekci I , Turan O . Energy and performance optimization of an adaptive cycle engine for next generation combat aircraft. Energy 2020; 209:118261.

[5]

Chen H , Zheng Q , Gao Y , Zhang H . Performance seeking control of minimum infrared characteristic on double bypass variable cycle engine. Aerosp Sci Technol 2021; 108:106359.

[6]

Sprouse JG . F—22 environmental control/thermal management system design optimization for reliability and integrity—a case study. In: SAE technical paper 961339. Warrendale: SAE International; 1996.

[7]

Tao Z , Fu Y , Xu G , Deng H , Jia Z . Experimental study on influences of physical factors to supercritical RP—3 surface and liquid—space thermal oxidation coking. Energy Fuels 2014; 28(9):6098-106.

[8]

Huang H , Spadaccini LJ , Sobel DR . Fuel—cooled thermal management for advanced aeroengines. J Eng Gas Turbine Power 2004; 126(2):284—93.

[9]

Lira A , Juarez R , Petersen EL , Loebick C . An experimental apparatus for controlled measurements to study fuel coking deposition at high temperatures. In: Proceedings of the AIAA SCITECH 2025 Forum; 2025 Jan 06—10; Orlando, FL, USA. Reston: American Institute of Aeronautics and Astronautics (AIAA);2025. p. 0745.

[10]

van Heerden AS , Judt DM , Jafari S , Lawson CP , Nikolaidis T , Bosak D . Aircraft thermal management: practices, technology, system architectures, future challenges, and opportunities. Prog Aerosp Sci 2022; 128:100767.

[11]

Jasa JP , Mader CA , Martins JR . Trajectory optimization of a supersonic aircraft with a thermal fuel management system. In: Proceedings of the 2018 Multidisciplinary Analysis and Optimization Conference; 2018 Jun 25—29; Atlanta, GA, USA. Reston: American Institute of Aeronautics and Astronautics Inc.; 2018. p. 3884.

[12]

Coutinho M , Bento D , Souza A , Cruz R , Afonso F , Lau F , et al. A review on the recent developments in thermal management systems for hybrid—electric aircraft. Appl Therm Eng 2023; 227:120427.

[13]

Kellermann H , Habermann A , Vratny P , Hornung M . Assessment of fuel as alternative heat sink for future aircraft. Appl Therm Eng 2020; 170:114985.

[14]

German BJ. Tank heating model for aircraft fuel thermal systems with recirculation. J Propuls Power 2012; 28(1):204-10.

[15]

Shi M , Gladin J , Mavris DN . A systematic methodology for populating the aircraft thermal management system architecture space. In: Proceedings of the AIAA SCITECH 2021 Forum; 2021 Jan 11—15; virtual event. Reston: American Institute of Aeronautics and Astronautics (AIAA); 2021. p. 1295.

[16]

Sigthorsson D , Oppenheimer MW , Doman DB . Aircraft thermal endurance enhancement using a dual tank configuration and temperature regulation. In: Proceedings of the 2018 AIAA Guidance, Navigation, and Control Conference; 2018 Jan 08—12; Kissimmee, FL, USA. Reston: American Institute of Aeronautics and Astronautics (AIAA); 2018. p. 0612.

[17]

Sigthorsson D , Oppenheimer MW , Doman DB . Flex versus dual tank thermal management systems. In: Proceedings of the AIAA SCITECH 2023 Forum; 2023 Jan 23—27; National Harbor, MD, USA. Reston: American Institute of Aeronautics and Astronautics (AIAA); 2023. p. 1045.

[18]

Sigthorsson D , Oppenheimer MW , Doman DB . N—tank thermal management system framework for thermal endurance enhancement. In: Proceedings of the AIAA SCITECH 2022 Forum; 2022 Jan 03—07; San Diego, CA, USA. Reston: American Institute of Aeronautics and Astronautics (AIAA); 2022. p. 0750.

[19]

Sigthorsson D , Oppenheimer MW , Doman DB . N—tank continuous framework for thermal management to enhance thermal endurance. In: Proceedings of the AIAA SCITECH 2024 Forum; 2024 Jan 08—12; Orlando, FL, USA. Reston: American Institute of Aeronautics and Astronautics (AIAA); 2024. p. 2202.

[20]

Huang GP , Doman DB , Oppenheimer MW , Tipton A , Sigthorsson DO . Control of a switched mode fuel thermal management system. J Thermophys Heat Trans 2022; 36(1):13-27.

[21]

Xu J , Wang R , Zhang Q , Cui T , Li H , Pei L , et al. Design of engine cooling system using improved particle swarm optimization algorithm. IEEE Sens J 2023; 23(17):19060-72.

[22]

Sigthorsson D , Oppenheimer MW , Doman DB . Flight endurance enhancement via thermal management system control subject to multiple limitations. In: Proceedings of the AIAA SCITECH 2020 Forum; 2020 Jan 06—10; Orlando, FL, USA. Reston: American Institute of Aeronautics and Astronautics (AIAA); 2020. p. 1825.

[23]

Doman DB. Rapid mission planning for aircraft thermal management. In: Proceedings of the AIAA Guidance, Navigation, and Control Conference; 2015 Aug 05—08; Boston, MA, USA. Reston: American Institute of Aeronautics and Astronautics (AIAA); 2015. p. 1076.

[24]

Doman DB. Fuel flow topology and control for extending aircraft thermal endurance. J Thermophys Heat Trans 2018; 32(1):35-50.

[25]

Wang H , Li P , Xiao H , Zhou X , Lei R . Intelligent energy management for solar—powered unmanned aerial vehicle using multi—objective genetic algorithm. Energy Convers Manage 2023; 280:116805.

[26]

Yang S , Lin Y , Yu H , Xu X , Liang X . Thermal management of fuel heat sink in aircraft via flow path optimization. Appl Therm Eng 2024; 246:122880.

[27]

Xu Y , Yan Z , Xia W . A novel system for aircraft cabin heating based on a vapor compression system and heat recovery from engine lubricating oil. Appl Therm Eng 2022; 212:118544.

[28]

Chen W , Wang R , Li X , Lu S , Fang X . Study of the heat transfer design of an integrated thermal management system for hypersonic vehicles using supercritical nitrogen as expendable coolant. Aerosp Sci Technol 2022; 123:107440.

[29]

Johnson DJ , Niedbalski NP , Ervin JS , Patnaik SS . A thermal management system using ammonium carbamate as an endothermic heat sink. Appl Therm Eng 2017; 121:897-907.

[30]

Wang Y , Xu Z , Wang H , Qiu Y , Cheng X , Bai J . Enhancing aerodynamic performance by waste heat in a hydrogen fuel cell powered aircraft. Appl Therm Eng 2024; 254:123873.

[31]

Corbett M. Shaft power extraction and waste heat rejection using a three stream variable cycle engine. SAE Int J Aerosp 2012; 5(2012—01—2167):371-85.

[32]

Dooley M , Lui N , Newman R , Lui C . Aircraft thermal management—heat sink challenge. Warrendale: SAE International; 2014.

[33]

Simmons RJ. Design and control of a variable geometry turbofan with an independently modulated third stream [dissertation]. Columbus: The Ohio State University;2009.

[34]

Clark RA , Shi M , Gladin J , Mavris D . Design and analysis of an aircraft thermal management system linked to a low bypass ratio turbofan engine. J Eng Gas Turbine Power 2022; 144(1):011019.

[35]

Walsh PP , Fletcher P . Gas turbine performance. Hoboken: John Wiley & Sons; 2004.

[36]

Xu G , Jia Z , Wen J , Deng H , Fu Y . Thermal—conductivity measurements of aviation kerosene RP—3 from (285 to 513) K at sub— and supercritical pressures. Int J Thermophys 2015; 36(4):620-32.

[37]

Fu Y , Gang X , Zhi H , Liu Y , Xu G . Isobaric specific heat capacity measurement in the trans—critical temperature regions for kerosene RP—3 under pressures of 6—8 MPa. J Chem Eng Data 2024; 69(11):3730-8.

[38]

Fu Y , Liu W , Shi S , Wang R , Liu Y , Xu G . Density measurements of aviation kerosene RP—3 over temperature range from 323 K to 783 K under supercritical pressures from 6 MPa to 8 MPa. Chin J Aeronauti 2025; 38(7):103474.

[39]

Liu Y , Xu G , Shi S , Wang R , Fu Y . Viscosity measurements of endothermic propellant EHF—TU and aviation kerosene RP—3 under supercritical pressures. J Chem Eng Data 2025; 70(2):827-34.

[40]

Huang C , Xu G , Wen J , Li M , Zhuang L . Performance advantage evaluation of air—oil heat exchanger based on variable cycle engine in flight mission. In: Proceedings of the ASME International Mechanical Engineering Congress and Exposition; 2022 Oct 30—Nov 3; Columbus, OH, USA. New York City: American Society of Mechanical Engineers (ASME); 2022. V008T011A025.

[41]

Cengel YA , Boles MA . Thermodynamics: an engineering approach. 7th ed. New York City: McGraw Hill; 2011.

[42]

Yang S , Tao W . Heat transfer. Beijing: Higher Education Press; 2006. Chinese.

[43]

Sojoudi A , Nourbakhsh A , Shokouhmand H . Experimental evaluation of temperature rise in centrifugal pumps at partial flow rates. J Braz Soc Mech Sci Eng 2018; 40(4):183.

[44]

Cengel YA , Boles MA . Engineering thermodynamics. 7nd ed. Shen W, Tong J, translators. Beijing: Higher Education Press; 2016.

[45]

Zhuang L, Xu G, Dong B, Liu Q, Huang C, Wen J. Study on performance and mechanisms of a novel integrated model with power & thermal management system and turbofan engine. Appl Therm Eng 2023; 219:119481.

[46]

Sekulic DP , Sekulic DP . Fundamentals of heat exchanger design. Hoboken: John Wiley & Sons; 2003.

[47]

Sha Z. Aircraft design manual. Beijing: Aerospace Industry Press; 2005. Chinese.

[48]

Mattingly JD . Aircraft engine design. 2nd ed. Reston: American Institute of Aeronautics and Astronautics (AIAA); 2002.

[49]

Shou R , He H . Aircraft environmental control. Beijing: Beihang University Press; 2004. Chinese.

[50]

Tipton R, Figliola RS, Ochterbeck JM. Thermal optimization of the ECS on an advanced aircraft with an emphasis on system efficiency and design methodology. In: SAE technical paper 971241. Warrendale: SAE International; 1997.

[51]

Tang M , Ji H , Hu Y . Optimal design of comprehensive thermal management system for supersonic vehicle. J Propuls Technol 2022; 43(1):50-60. Chinese.

PDF (3516KB)

0

Accesses

0

Citation

Detail

Sections
Recommended

/