180 results on '"Nie, Wansheng"'
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2. Experimental and numerical study of nonlinear growth process of self-excited combustion instability in a model rocket combustor
3. Experimental and numerical investigation of transverse combustion instability in a rectangle multi-injector rocket combustor
4. Experimental research on micro thrust measurement of ion thruster under variable working conditions
5. Detection of Precursors of Thermoacoustic Instability in a Swirled Combustor Using Chaotic Analysis and Deep Learning Models
6. Experimental Study of the Effect of the Initial Droplet Diameter on the Evaporation Characteristics of Unsymmetrical Dimethylhydrazine Droplets in a Subcritical Environment
7. Early detection of thermoacoustic instability in an O2/CH4 single-injector rocket combustor using analysis of chaos and deep learning models
8. Mixing enhancement mechanism of combined H2–Water jets in supersonic crossflows in a combustor with an expanded section
9. Numerical simulation of single/double liquid jets in supersonic crossflows
10. Research on nonequilibrium plasma-assisted evaporation and ignition of n-decane droplet.
11. Analysis of spontaneous longitudinal combustion instability in an O2/CH4 single-injector rocket combustor
12. Experimental study of the evaporation characteristics of unsymmetrical dimethylhydrazine in a sub-supercritical environment
13. Numerical investigation on spray self-pulsation characteristics of a liquid-centered swirl coaxial injector
14. Numerical investigation of spray self-pulsation characteristics of liquid-centered swirl coaxial injector with different recess lengths
15. Atomization of a liquid jet in supersonic crossflow in a combustion chamber with an expanded section
16. High frequency combustion instability control by discharge plasma in a model rocket engine combustor
17. Early detection of thermoacoustic instability in an O2/CH4 single-injector rocket combustor using analysis of chaos and deep learning models.
18. Three-Dimensional Numerical Analysis of Longitudinal Thermoacoustic Instability in a Single-Element Rocket Combustor
19. Characterization of the effects of a plasma injector driven by AC dielectric barrier discharge on ethylene-air diffusion flame structure
20. Structures and aero-optical effects of supersonic flow over a backward facing step with vortex generators
21. Influence of equivalence ratio on plasma assisted detonation initiation by alternating current dielectric barrier discharge under rich burn condition
22. Plasma-assisted flame stabilization by AC dielectric barrier discharge in burst mode.
23. Numerical analysis of self-excited tangential combustion instability for an MMH/NTO rocket combustor.
24. Plasma-Assisted Combustion
25. Experimental Research on Micro Thrust Measurement of Ion Thruster Under Variable Working Conditions
26. Experimental and Numerical Investigation of Transverse Combustion Instability in 2d Multi-Injector Rocket Combustor
27. Rotating detonation combustion of liquid kerosene under near-ramjet limit conditions.
28. Tangential stretching rate analysis of DRGEP-based automated target species selection dynamic adaptive chemistry method.
29. Numerical Simulation of the Atomization Process of a Like-doublet Impinging Rocket Injector
30. Numerical analysis of self-excited tangential combustion instability for an MMH/NTO rocket combustor
31. Wide-Range Displacement Sensor for Vibration Measurement of Magnetically Suspended Air-Blower
32. Vibration Analysis and Active Control of Rotor Shaft in Magnetically Suspended Air-Blower
33. Measurement and diagnosis of miniaturized ion thruster plume.
34. Experimental studies the burning process of gelled unsymmetrical dimethylhydrazine droplets under oxidant convective conditions
35. High frequency combustion instability control by discharge plasma in a model rocket engine combustor
36. The Effects of Non-uniform Distribution of Oxidizer Flow on High-Frequency Combustion Instability
37. Migration and Evaporation Characteristics of Kerosene Droplet in Supercritical Environment
38. Numerical Investigation on Spray Characteristics With Upstream Flow Pulsation of a Pintle Injector
39. Analysis of self-excited transverse combustion instability in a rectangular model rocket combustor
40. Modeling, simulation and experimental study of squeeze engine system
41. Numerical simulation of similarities between rotating detonation and high-frequency combustion instability under two mixing schemes
42. Analysis of Tangential Combustion Instability Modes in a LOX/Kerosene Liquid Rocket Engine Based on OpenFOAM
43. Study of thrust vector control for the rotating detonation model engine
44. Experimental investigation on effects of injection distribution on combustion instability in a model rocket combustor
45. Influence of Self-Pulsation on Atomization Characteristics of Gas-Centered Swirl Coaxial Injector
46. Influence of Self-Pulsation on Atomization Characteristics of Gas-Centered Swirl Coaxial Injector
47. Simulation of a liquid jet in supersonic crossflow by a hybrid CLSVOF-LPT method
48. Propagation Mode Analysis on H2–Air Rotating Detonation Waves in a Hollow Combustor
49. Structures of liquid jets in supersonic crossflows in a rectangular channel with an expansion section
50. The role of non-equilibrium plasma kinetic effect on GCH4/GOX rocket engine combustion performance
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