Employment
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Education
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Nanjing University of Aeronautics and Astronautics
Projects & Funding
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Publications (12)
- Experimental investigation on unstart-restart hysteresis of a supersonic inlet during throat regulation Save
- Unstart/Restart Boundary Broadening Method for a Two-Dimensional Supersonic Variable Inlet Based on a Distributed Bleed System Save
- Suppression of flow response hysteresis in the throttling/unthrottling process for supersonic inlet Save
- A real-time online unstart prediction approach for supersonic inlet Save
- Comparative study on single-incident and dual-incident shock wave/turbulent boundary layer interactions with identical total deflection angle Save
- Throttling Characteristics of a Supersonic Variable Inlet at Different Internal Contraction Ratios Save
- Oscillations in Rectangular Supersonic Inlets with Large Internal Contraction Ratio Save
- Flow response hysteresis of throat regulation process of a two-dimensional mixed-compression supersonic inlet Save
- Feasibility of employing the restarting process to evaluate the self-starting ability for hypersonic inlets Save
- Prediction of self-starting limit of two-dimensional supersonic inlets considering viscous effects Save