12 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. Longitudinal combustion instability in a hypergolic liquid bipropellant combustor with single dual-swirl coaxial injector
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 investigation of spray self-pulsation characteristics of liquid-centered swirl coaxial injector with different recess lengths
8. Atomization of a liquid jet in supersonic crossflow in a combustion chamber with an expanded section
9. High frequency combustion instability control by discharge plasma in a model rocket engine combustor
10. Numerical Simulation of the Atomization Process of a Like-doublet Impinging Rocket Injector
11. Experimental studies the burning process of gelled unsymmetrical dimethylhydrazine droplets under oxidant convective conditions
12. Simulation of a liquid jet in supersonic crossflow by a hybrid CLSVOF-LPT method
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