Volume 41 Issue 4
Apr.  2026
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XIONG Tuan, LIN Shangchao, HE Miaosheng, et al. Research on solid-state thermoelectric generation technology utilizing aerodynamic heat at leading edge of hypersonic vehicles[J]. Journal of Aerospace Power, 2026, 41(4):20250109 doi: 10.13224/j.cnki.jasp.20250109
Citation: XIONG Tuan, LIN Shangchao, HE Miaosheng, et al. Research on solid-state thermoelectric generation technology utilizing aerodynamic heat at leading edge of hypersonic vehicles[J]. Journal of Aerospace Power, 2026, 41(4):20250109 doi: 10.13224/j.cnki.jasp.20250109

Research on solid-state thermoelectric generation technology utilizing aerodynamic heat at leading edge of hypersonic vehicles

doi: 10.13224/j.cnki.jasp.20250109
  • Received Date: 2025-03-06
    Available Online: 2025-06-16
  • Focusing on aerodynamic heat recovery challenges in hypersonic vehicles, the solid-state thermoelectric power generation technology at the leading edge for blunt-body vehicle architectures was investigated. A multi-physics computational model integrating hypersonic vehicles with thermoelectric generators was developed to simulate the electrical output characteristics under actual high-altitude flight conditions. The accuracy of the model was verified through ground platform tests and wind tunnel tests, while the output performance of thermoelectric generators under different environmental conditions was systematically examined. Comparative studies were conducted on thermoelectric devices with various materials and configurations. The results revealed that the thermoelectric generators effectively converted aerodynamic heat into electrical energy, with a single TEG achieving maximum output power of 1.21 W and power density of 1344.44 W/m2 under simulated actual flight conditions. Wind tunnel test demonstrated closer approximation to real flight environments compared with ground platform tests, as it yielded a maximum output power of 0.5 W and peak conversion efficiency of 2.58% for individual TEG. Thermoelectric materials in different temperature zones were suited to distinct TEG structures, requiring rational design and arrangement to optimize the performance.

     

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