Jiangfei Yu

National University of Defense Technology — China

Engineering · Physical Sciences

16h-index925citations37works15.82yr avg
OpenAlex↗ORCID↗Google Scholar↗Lab page↗

Accepting Students?

No reports yet. Know if this professor is taking students?

Research Topics

Combustion and flame dynamics(27), Computational Fluid Dynamics and Aerodynamics(23), Fluid Dynamics and Turbulent Flows(16), Advanced Combustion Engine Technologies(9), Aerodynamics and Acoustics in Jet Flows(7)

Publications37 total

Effect of CO on the propagation of natural gas flames with heat flux burner
Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering·2026
An experimental investigation of heat transfer phenomena in shock wave/boundary layer interaction at Mach 6
Aerospace Science and Technology·2025· 4 citedOpen Access
Local Mixture Stratification Modulates Detonation Characteristics and Combustion Performance in a Dual-Channel Combustor
SSRN Electronic Journal·2025Open Access
Flow structures and combustion regimes in an axisymmetric scramjet combustor with high Reynolds number
Journal of Fluid Mechanics·2024· 31 citedOpen Access
Investigation of multi-scale flow structures and combustion characteristics in a cavity-enhanced circular scramjet
Combustion and Flame·2024· 44 cited
Analysis of influencing factors on numerical simulation of transverse jet in supersonic flow
Advances in Mechanical Engineering·2023· 1 citedOpen Access
Study on the application of artificial neural network-based flamelet/progress variable model in supersonic combustion
AIP Advances·2023· 1 citedOpen Access
Flamelet-like models applied in scramjet combustors: A state of art and prospect
Chinese Journal of Aeronautics·2023· 12 citedOpen Access
An improved flamelet/progress variable modeling in a hydrogen-fueled scramjet
International Journal of Hydrogen Energy·2023· 13 cited
Numerical study of transverse jet mixing and combustion in a high-enthalpy supersonic crossflow with trace gases
Physics of Fluids·2023· 32 cited
The nature of sawtooth wave and its distinction from continuous rotating detonation wave
Proceedings of the Combustion Institute·2022· 13 cited
A method for optimizing reaction progress variable and its application
Aerospace Science and Technology·2022· 7 cited
Effect of injection scheme on asymmetric phenomenon in rectangular and circular scramjets
Chinese Journal of Aeronautics·2022· 33 citedOpen Access
Evaluation of flamelet/progress variable model for the applications in supersonic combustion using hybrid RANS/LES approach
Aerospace Science and Technology·2022· 12 cited
Effects of confinement and curvature on a jet in a supersonic cross-flow
Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering·2022· 23 cited
Numerical Investigation of Contact Burning in an Air-Breathing Continuous Rotating Detonation Engine
International Journal of Aerospace Engineering·2022· 8 citedOpen Access
Mechanism of development of turbulent boundary layer in a curved circular pipe under supersonic conditions
AIP Advances·2022· 7 citedOpen Access
Numerical and theoretical investigation of ethanol/air flame instability
Combustion Theory and Modelling·2020· 28 cited
Effect of the Backward Facing Step on a Transverse Jet in Supersonic Crossflow
Energies·2020· 10 citedOpen Access
Turbulent boundary layer subjected to a sonic transverse jet in a supersonic flow
Aerospace Science and Technology·2020· 20 cited
page 1 of 2Next →

Frequent Co-authors

Mingbo Sun(26), Hongbo Wang(19), Tao Tang(9), Yixin Yang(9), Guoyan Zhao(8), Zhenguo Wang(7), Dapeng Xiong(7), Xue‐Song Bai(6), Rixin Yu(5), Zhenguo Wang(5), Yuhui Huang(5), Changhai Liang(5), Chaoyang Liu(4), Weidong Liu(4), Haoyang Peng(3), Yu-Hui Huang(2), Yuan Liu(2), Guangxin Li(2), Shijie Liu(2), Jincheng Zhang(2)