236 results on '"Xu, Jinglei"'
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2. Mapping the landscape: a bibliometric analysis of resting-state fMRI research on schizophrenia over the past 25 years
3. Corrected Navier-Stokes equations for compressible flows
4. Lattice eddy simulation of turbulent flows
5. Numerical investigation of dynamic characteristics of dual throat nozzle and bypass dual throat nozzle in thrust vectoring starting process
6. A parametric investigation of Dual-throat nozzle bypass channel configurations for advanced Aviation applications
7. Numerical investigations of different liner lengths of axial film cooling for a rotating detonation engine
8. Evaluation and analysis of carbon neutralization capacity in the Yangtze River Economic Belt: Based on time weighted-rough set and unascertained model
9. Numerical simulation and experiment of a bypass dual throat nozzle with tab modification
10. Large-eddy simulation of unsteady flows past a spiked body
11. Experimental investigation of flow unsteadiness over four types of spiked-blunt body at Mach 2.2
12. Numerical investigation of short takeoff and landing exhaust system using bypass dual throat nozzle
13. Numerical investigations of the nozzle performance for a rocket-based rotating detonation engine with film cooling
14. Numerical study of a trapezoidal bypass dual throat nozzle
15. Experimental investigation of the distorted flow field in a new type of direct-connect facility for scramjet studies
16. Experimental investigation of the pulsing flow field around four types of spiked-blunt body at Mach 2.2
17. Numerical investigation of the shock-focusing detonation engines with different nozzle configurations
18. Modular design framework of an axisymmetric wrap-around thrust-optimized combined nozzle
19. Extension of the KDO turbulence/transition model to account for roughness
20. Design and experimental study of a bypass dual throat nozzle with the ability of short/vertical takeoff and landing
21. Morphological and nanostructure characteristics of soot particles emitted from a jet-stirred reactor burning aviation fuel
22. Numerical Study of Discrete Hole Supersonic Film Cooling with Shock Generator
23. Experimental Investigation of the Shock-Related Unsteadiness around a Spiked-Blunt Body Based on a Novel DMD Energy Sorting Criterion
24. Experimental validation of a new type of direct-connect facility for scramjet studies
25. Experimental verification of pulsation suppression over spiked cylinder using standard/double/inverse aerodome
26. The initial flow structures and oscillations of an underexpanded impinging jet
27. Design and analysis of the scramjet nozzle with contact discontinuity
28. Flow instability and asymmetry over spiked cylinder
29. Assessment of pressure field and performance parameter reconstruction from velocity data for ramjet inlet
30. Experimental and numerical investigations on the mode transition process of an exhaust system for an over-under turbine based combined cycle
31. Numerical study of supersonic turbulent boundary layer combustion with pressure gradient
32. Optimization and analysis of inverse design method of maximum thrust scramjet nozzles
33. Suppression and utilisation of aeroelastic behaviour in turbine-based combined cycle inlet
34. An anisotropic turbulence model for predicting heat transfer in a rotating channel
35. Experimental and numerical investigations of a scramjet nozzle at various operations
36. Distribution of stress intensity ratio in canonical turbulent flows and converging-diverging channel
37. Inverse design method on scramjet nozzles based on maximum thrust theory
38. Numerical simulation and experiment of a bypass dual throat nozzle with tab modification
39. Maximum-Thrust Nozzle Based on Height Constraints
40. Design and performance analysis of an exhaust system for an over-under turbine based combined cycle operating at Mach 0–6
41. Inverse design methodology on a single expansion ramp nozzle for scramjets
42. Role of aerodome in pulsation/oscillation control and aeroheating reduction
43. Aeroheating reduction for blunt body using aerodome jet
44. Inverse design methodology of cone-derived waverider based on pre-defined shock wave under strong geometric constraints
45. Effect of adverse pressure gradient on supersonic compressible boundary layer combustion
46. Computational study of axisymmetric divergent bypass dual throat nozzle
47. Numerical evaluation of aerodome and cooling jet for aeroheating reduction
48. Capturing transition with flow–structure–adaptive KDO RANS model
49. Mean flow compressibility effects in transonic turbulence modeling
50. Starting characteristics and phenomenon of a supersonic wind tunnel coupled with inlet model
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