84 results on '"Nie, Wansheng"'
Search Results
2. Experimental Study of the Effect of the Initial Droplet Diameter on the Evaporation Characteristics of Unsymmetrical Dimethylhydrazine Droplets in a Subcritical Environment
3. Early detection of thermoacoustic instability in an O2/CH4 single-injector rocket combustor using analysis of chaos and deep learning models
4. Experimental study of the evaporation characteristics of unsymmetrical dimethylhydrazine in a sub-supercritical environment
5. Experimental research on micro thrust measurement of ion thruster under variable working conditions
6. Experimental and numerical investigation of transverse combustion instability in a rectangle multi-injector rocket combustor
7. Plasma-Assisted Combustion
8. Experimental Research on Micro Thrust Measurement of Ion Thruster Under Variable Working Conditions
9. Experimental and Numerical Investigation of Transverse Combustion Instability in 2d Multi-Injector Rocket Combustor
10. Numerical analysis of self-excited tangential combustion instability for an MMH/NTO rocket combustor
11. Wide-Range Displacement Sensor for Vibration Measurement of Magnetically Suspended Air-Blower
12. Vibration Analysis and Active Control of Rotor Shaft in Magnetically Suspended Air-Blower
13. Numerical Investigation on Spray Characteristics With Upstream Flow Pulsation of a Pintle Injector
14. Analysis of self-excited transverse combustion instability in a rectangular model rocket combustor
15. Mixing enhancement mechanism of combined H2–Water jets in supersonic crossflows in a combustor with an expanded section
16. Modeling, simulation and experimental study of squeeze engine system
17. Numerical simulation of similarities between rotating detonation and high-frequency combustion instability under two mixing schemes
18. Analysis of Tangential Combustion Instability Modes in a LOX/Kerosene Liquid Rocket Engine Based on OpenFOAM
19. Study of thrust vector control for the rotating detonation model engine
20. Experimental investigation on effects of injection distribution on combustion instability in a model rocket combustor
21. Numerical simulation of single/double liquid jets in supersonic crossflows
22. Analysis of spontaneous longitudinal combustion instability in an O2/CH4 single-injector rocket combustor
23. Plasma-assisted flame stabilization by AC dielectric barrier discharge in burst mode
24. Influence of Self-Pulsation on Atomization Characteristics of Gas-Centered Swirl Coaxial Injector
25. Simulation of a liquid jet in supersonic crossflow by a hybrid CLSVOF-LPT method
26. Numerical investigation on spray self-pulsation characteristics of a liquid-centered swirl coaxial injector
27. Numerical investigation of spray self-pulsation characteristics of liquid-centered swirl coaxial injector with different recess lengths
28. Atomization of a liquid jet in supersonic crossflow in a combustion chamber with an expanded section
29. High frequency combustion instability control by discharge plasma in a model rocket engine combustor
30. Propagation Mode Analysis on H2–Air Rotating Detonation Waves in a Hollow Combustor
31. Structures of liquid jets in supersonic crossflows in a rectangular channel with an expansion section
32. The role of non-equilibrium plasma kinetic effect on GCH4/GOX rocket engine combustion performance
33. Characterization of the effects of a plasma injector driven by AC dielectric barrier discharge on ethylene-air diffusion flame structure
34. Study of plasma-assisted detonation initiation by quasi-direct current discharge
35. Experimental Investigation of CH4/Air Inverse Diffusion Flame Stabilization by Nonequilibrium Plasma
36. Experimental study on the diffusive flame stabilization mechanism of plasma injector driven by AC dielectric barrier discharge
37. Experimental investigation of thermodynamic instability of supercritical endothermic hydrocarbon fuel within a small-scale channel
38. Structures and aero-optical effects of supersonic flow over a backward facing step with vortex generators
39. The Effects of Non-uniform Distribution of Oxidizer Flow on High-Frequency Combustion Instability
40. Migration and Evaporation Characteristics of Kerosene Droplet in Supercritical Environment
41. Numerical study of plasma assisted combustion for a rocket combustor using GCH4/GOX as propellants
42. Study on the Cooling Characteristics of the Liquid Oxygen Kerosene Engine Exhaust Plume Impact by the Water Injection
43. Calculation of Characteristic Parameters of Solid Rocket Exhaust Plume Plasma
44. Investigation on the Mechanism of Thermoacoustic Instability of n-Decane at Subcritical Pressure
45. Effect of actuating voltage and discharge gap on plasma assisted detonation initiation process
46. Influence of equivalence ratio on plasma assisted detonation initiation by alternating current dielectric barrier discharge under rich burn condition
47. Study on the influence of actuation parameter of SDBD on induced jet in low-pressure air
48. Influence of deflector on impact properties of multi-nozzle LOX/kerosene engine exhaust plume
49. Numerical simulation of high frequency instability induced by the distribution of gas-liquid scheme injectors in an experiment-scale Kero/GOX liquid rocket engine
50. A Kind of Model-rocket Combustor Test Bed
Catalog
Books, media, physical & digital resources
Discovery Service for Jio Institute Digital Library
For full access to our library's resources, please sign in.