25 results on '"Nie, Wansheng"'
Search Results
2. Calculation of Characteristic Parameters of Solid Rocket Exhaust Plume Plasma
3. The Effects of Non-uniform Distribution of Oxidizer Flow on High-Frequency Combustion Instability.
4. Migration and Evaporation Characteristics of Kerosene Droplet in Supercritical Environment.
5. Influence of deflector on impact properties of multi-nozzle LOX/kerosene engine exhaust plume
6. Numerical simulation of high frequency instability induced by the distribution of gas-liquid scheme injectors in an experiment-scale Kero/GOX liquid rocket engine
7. Numerical Simulation of Damping Capacity between Injector-Formed Baffle and Normal Blade Baffle in a Kero/LOX Liquid Rocket Engine
8. Experiment on Jet Flow Control by SDBD Plasma Actuator
9. Numerical Study of Non-Equilibrium Plasma Assisted Combustion on Spacecraft Rocket Engine
10. Three Dimensional Numerical Simulation for the Effect of Quasi-DC Plasma on Ethylene-Air Jet Flow In Scramjet Combustor
11. Numerical Study of the Influence of the Opening Ratio on the Damping Capacity of the Injector
12. Numerical Study of the acoustic characteristics of the entry diameter gas-liquid coaxial swirling injector
13. The Effects of Weber Numbers on Central Collision Between Two Droplets
14. Effects of NTO Oxidizer Convection Velocity and Pressure on the Combustion Characteristics of UDMH Nonmetalized Organic Gel Droplet: Experimental Studies
15. Effects of NTO Oxidizer Convection Velocity and Pressure on the Combustion Characteristics of UDMH Nonmetalized Organic Gel Droplet: Numerical Studies
16. Experimental Investigation of Atomization and Combustion of Gelled Propellant in High-pressure Oxidant Environment
17. Experimental Investigation of Atomization and Combustion of Organic Gel Propellant
18. Vaporization and Combustion of LOX Droplets at Supercritical Conditions
19. A Numerical Study of Oxygen/Hydrogen Mixing and Combustion of a Shear Coaxial Injector
20. Three-Dimensional Numerical Simulations of Low Frequency Combustion Instability in a LOX/Methane Rocket Engine
21. Combustion Instability Analysis in a Hydrogen-Oxygen Rocket Engine
22. Effects Investigation of Physical Models on Combustion Processes of LOX/GH2 Rocket Engine
23. Predictor-corrector terminal guidance logic of gliding vehicle with final states constraints.
24. Numerical simulation of MMH/NTO rocket engine combustion instability
25. Liquid rocket combustion instability analysis methodology - Methods and representative examples
Catalog
Books, media, physical & digital resources
Discovery Service for Jio Institute Digital Library
For full access to our library's resources, please sign in.