De-kun Yan

Thermal analysis of regenerative-cooled pylon in multi-mode rocket based combined cycle engine

F. Qin, G. He, Wenqiang Li, 2018, Acta Astronautica.

Effect of area ratio and heat release method on the Ma∞ = 2-6 operation performance of rocket-based combined cycle engine

R. Martinuzzi, F. Qin, G. He, 2022, Aerospace Science and Technology.

Ejector mode performance improvement of rocket-based combined cycle engine designed for dual-ramjet mode

R. Martinuzzi, G. He, De-kun Yan, 2022, Aerospace Science and Technology.

Analysis and reduction of skin-friction in a rocket-based combined-cycle engine flow path operating from Mach 1.5 to 6.0

Guoqiang He, Zhiwei Huang, Fei Qin, 2018, Acta Astronautica.

Effect of the heat release on the component coordination in the rocket-based combined cycle engine

Guoqiang He, Fei Qin, Dekun Yan, 2018, Acta Astronautica.