17 results on '"Nie, Wansheng"'
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2. A polynomial temperature profile model for suspended droplet evaporation over a wide range of ambient pressures and convection conditions
3. Experimental and numerical study of nonlinear growth process of self-excited combustion instability in a model rocket combustor
4. Experimental and numerical investigation of transverse combustion instability in a rectangle multi-injector rocket combustor
5. Experimental research on micro thrust measurement of ion thruster under variable working conditions
6. Mixing enhancement mechanism of combined H2–Water jets in supersonic crossflows in a combustor with an expanded section
7. Numerical simulation of single/double liquid jets in supersonic crossflows
8. Analysis of spontaneous longitudinal combustion instability in an O2/CH4 single-injector rocket combustor
9. Numerical investigation on spray self-pulsation characteristics of a liquid-centered swirl coaxial injector
10. Numerical investigation of spray self-pulsation characteristics of liquid-centered swirl coaxial injector with different recess lengths
11. Atomization of a liquid jet in supersonic crossflow in a combustion chamber with an expanded section
12. High frequency combustion instability control by discharge plasma in a model rocket engine combustor
13. Structures and aero-optical effects of supersonic flow over a backward facing step with vortex generators
14. Influence of equivalence ratio on plasma assisted detonation initiation by alternating current dielectric barrier discharge under rich burn condition
15. Numerical Simulation of the Atomization Process of a Like-doublet Impinging Rocket Injector
16. Experimental studies the burning process of gelled unsymmetrical dimethylhydrazine droplets under oxidant convective conditions
17. Simulation of a liquid jet in supersonic crossflow by a hybrid CLSVOF-LPT method
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