151. Flow-field analysis and pressure gain estimation of a rotating detonation engine with banded distribution of reactants
- Author
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Jian-Ping Wang, Xiang-Yang Liu, Yan-Liang Chen, and Ming-Yi Luan
- Subjects
Renewable Energy, Sustainability and the Environment ,Detonation ,Energy Engineering and Power Technology ,02 engineering and technology ,Mechanics ,Solver ,010402 general chemistry ,021001 nanoscience & nanotechnology ,Condensed Matter Physics ,Combustion ,01 natural sciences ,0104 chemical sciences ,Physics::Fluid Dynamics ,Reaction rate ,Fuel Technology ,Combustion chamber ,0210 nano-technology ,Reynolds-averaged Navier–Stokes equations ,Stagnation pressure ,Longitudinal wave - Abstract
The flow-field structure and pressure gain performance of a rotating detonation engine with banded distribution of reactants have been studied using two-dimensional numerical simulations. The reactants are premixed H2/Air mixture. An unsteady reacting flow solver named rhoHLLCFoam is developed based on the open source software OpenFOAM. Unsteady Reynolds Averaged Navier-Stokes (RANS) equations are solved with second order accuracy in space and time with Harten-Lax-van-Leer-Contact (HLLC) Riemann scheme. The solver resolves the combustion phenomena through finite rate chemistry reaction model with Arrhenius form of reaction rate by using O Conaire scheme. After checking the reliability of the solver, two sets of cases with various inlet-area ratios (ψ) and equivalence ratios (ϕ) are conducted. The result shows that with ψ 1.0 , the reactants in front of detonation waves present a discretely banded distribution which causes a series of reverse compression waves in flow-field. This paper estimates the specific impulse and specific thrust of combustion chamber. It's shown that these parameters increase with the promotion of ψ. By calculating the area-averaged stagnation pressure along axial direction of combustion chamber, the pressure gain ratio (η) of the rotating detonation engine is estimated. The result suggests that η decreases dramatically with the reduction of ψ. In order to achieve pressure gain, ψ must be greater than 0.60. Moreover, the equivalence ratio should be around unity to obtain higher value of η.
- Published
- 2020