journal article·2021-08-01Open access

Influence of flow parameters on single shock-wave-focusing detonation and initial verification

Hesong Zhang, Xin Chen, Shida Xu, Dongliang Bian

AIP Advances· Volume 11· Issue 8

Abstract

As an advanced method for initiating detonation, shock-wave focusing (SWF) can do so directly without a separate igniter, and the distance of focusing initiation is much smaller than that of the deflagration-to-detonation transition, thereby greatly improving the performance of detonation engines. In this paper, the process of SWF detonation initiation with decane as the fuel is simulated, and it is found that the energy in the focusing region is high enough to initiate detonation directly. The total temperature and pressure of the incident flow are changed to study how the inlet parameters influence SWF. It is found that the total pressure of the incoming flow affects the SWF considerably whereas the influence of the total temperature can be ignored. The experimental results show that a kerosene–air detonation can be initiated successfully by SWF, thereby verifying the feasibility of SWF detonation with no pre-combustion chamber or igniter. The simulation and experimental results show that SWF detonation initiation has considerable advantages and potential.
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Research context

OpenAlex topics: Combustion and Detonation Processes · Energetic Materials and Combustion · Fire dynamics and safety research

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University , Xi’an 710038, China

Funding

National Natural Science Foundation of China

References (26)

Show source-provided references
1. 1986
2. 1996
3. Detonation database
4. Flame acceleration and deflagration-to-detonation transition in micro- and macro-channels: An integrated mechanistic study10.1016/j.combustflame.2016.10.010 ↗
5. High speed turbulent deflagrations and transition to detonation in H2–air mixtures10.1016/0010-2180(84)90039-7 ↗
6. Experimental evaluation of a two-stage pulse detonation combustor
7. Acceleration of DDT by non-thermal plasma in a single-trial detonation tube10.1016/j.cja.2017.12.016 ↗
8. A new approach to organizing operation cycles in pulse detonation engines
9. Reflection of a plane shock wave from a rigid concave wall10.1007/BF01015024 ↗
10. Detonation and deflagration initiation at the focusing of shock waves in combustible gaseous mixture10.1007/s001930050007 ↗
11. Spectra signals of gas pressure pulsations in annular and linear dual-slotted nozzles10.1080/00102202.2018.1467405 ↗
12. Investigation of the spectral composition of the gas pressure and thrust pulsations in nozzles equipped with a deflector10.1134/s0015462819030017 ↗
13. A compact shock-focusing geometry for detonation initiation: Experiments and adjoint-based variational data assimilation10.1016/j.combustflame.2017.03.014 ↗
14. Numerical investigation on detonation initiation using toroidal shock wave focusing10.1016/j.ast.2019.06.016 ↗
15. Detonation initiation via imploding shock waves in a tube
16. Detonation initiation via imploding shock waves
17. Initiation of detonations and deflagrations by shock reflection and focusing
18. Detonation initiation in a tube via imploding toroidal shock waves10.2514/1.35569 ↗
19. The dynamics of combustion products’ flow in a ring nozzle with a half-closed cavity10.1080/00102202.2010.501613 ↗
20. Gas dynamics and thrust in the exhaust system of a jet engine with an annular nozzle10.1134/s0010508212040053 ↗
21. Investigating an annular nozzle on combustion products of hydrocarbon fuels10.1134/s0869864313030013 ↗
22. Detonation onset following shock wave focusing10.1016/j.actaastro.2016.09.014 ↗
23. Onset of detonation in hydrogen-air mixtures due to shock wave reflection inside a combustion chamber10.1016/j.actaastro.2018.05.024 ↗
24. Investigation on shock wave focusing in 2-stage PDE
25. Investigation of the annular nozzle start in actual and virtual intermittent aerodynamic setups10.1134/s0015462816020150 ↗
26. Direct initiation of gaseous detonation by interacting supersonic jets10.1007/978-94-011-5432-1_30 ↗