Generation and Propagation Characteristics of an Auto-Ignition Flame Kernel Caused by the Oblique Shock in a Supersonic Flow Regime
被引:2
作者:
Xi, Wenxiong
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Cent South Univ, Sch Aeronaut & Astronaut, Changsha 410012, Peoples R ChinaCent South Univ, Sch Aeronaut & Astronaut, Changsha 410012, Peoples R China
Xi, Wenxiong
[1
]
Xu, Mengyao
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Cent South Univ, Sch Aeronaut & Astronaut, Changsha 410012, Peoples R ChinaCent South Univ, Sch Aeronaut & Astronaut, Changsha 410012, Peoples R China
Xu, Mengyao
[1
]
Liu, Chaoyang
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Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410015, Peoples R ChinaCent South Univ, Sch Aeronaut & Astronaut, Changsha 410012, Peoples R China
Liu, Chaoyang
[2
]
Liu, Jian
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Cent South Univ, Sch Aeronaut & Astronaut, Changsha 410012, Peoples R ChinaCent South Univ, Sch Aeronaut & Astronaut, Changsha 410012, Peoples R China
Liu, Jian
[1
]
Sunden, Bengt
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Cent South Univ, Sch Aeronaut & Astronaut, Changsha 410012, Peoples R China
Lund Univ, Dept Energy Sci, POB 118, SE-22100 Lund, SwedenCent South Univ, Sch Aeronaut & Astronaut, Changsha 410012, Peoples R China
Sunden, Bengt
[1
,3
]
机构:
[1] Cent South Univ, Sch Aeronaut & Astronaut, Changsha 410012, Peoples R China
[2] Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410015, Peoples R China
[3] Lund Univ, Dept Energy Sci, POB 118, SE-22100 Lund, Sweden
The auto-ignition caused by oblique shocks was investigated experimentally in a supersonic flow regime, with the incoming flow at a Mach number of 2.5. The transient characteristics of the auto-ignition caused by shock evolvements were recorded with a schlieren photography system, and the initial flame kernel generation and subsequent propagation were recorded using a high-speed camera. The fuel mixing characteristics were captured using NPLS (nanoparticle-based planar laser scattering method). This work aimed to reveal the flame spread mechanism in a supersonic flow regime. The effects of airflow total temperature, fuel injection pressure, and cavity length in the process of auto-ignition and on the auto-ignitable boundary were investigated and analyzed. From this work, it was found that the initial occurrence of auto-ignition is first induced by oblique shocks and then propagated upstream to the recirculation region, to establish a sustained flame. The auto-ignition performance can be improved by increasing the injection pressure and airflow total temperature. In addition, a cavity with a long length has benefits in controlling the flame spread from the induced state to a sustained state. The low-speed recirculating region created in the cavity is beneficial for the flame spread, which has the function of flame-holding and prevents the flame from being blown away.
机构:
Lincoln Univ Coll, Fac Engn, Petaling Jaya 47301, MalaysiaLincoln Univ Coll, Fac Engn, Petaling Jaya 47301, Malaysia
Athithan, A. Antony
;
Jeyakumar, S.
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Lincoln Univ Coll, Fac Engn, Petaling Jaya 47301, Malaysia
Kalasalingam Acad Res & Educ, CFD Ctr, Aeronaut Engn, Krishnankoil 626126, IndiaLincoln Univ Coll, Fac Engn, Petaling Jaya 47301, Malaysia
Jeyakumar, S.
;
Sczygiol, Norbert
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Czestochowa Tech Univ, Fac Mech Engn & Comp Sci, PL-42201 Czestochowa, PolandLincoln Univ Coll, Fac Engn, Petaling Jaya 47301, Malaysia
Sczygiol, Norbert
;
Urbanski, Mariusz
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Czestochowa Tech Univ, Fac Civil Engn, PL-42201 Czestochowa, PolandLincoln Univ Coll, Fac Engn, Petaling Jaya 47301, Malaysia
Urbanski, Mariusz
;
Hariharasudan, A.
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Kalasalingam Acad Res & Educ, Fac English, Krishnankoil 626126, IndiaLincoln Univ Coll, Fac Engn, Petaling Jaya 47301, Malaysia
机构:
Seoul Natl Univ, Dept Aerosp Engn, Seoul 08826, South KoreaSeoul Natl Univ, Dept Aerosp Engn, Seoul 08826, South Korea
Jeong, Eunju
;
O'Byrne, Sean
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Univ New South Wales, Australian Def Force Acad, Sch Aerosp & Mech Engn, Canberra, ACT 2600, AustraliaSeoul Natl Univ, Dept Aerosp Engn, Seoul 08826, South Korea
O'Byrne, Sean
;
Jeung, In-Seuck
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Seoul Natl Univ, Dept Aerosp Engn, Seoul 08826, South Korea
Seoul Natl Univ, Inst Adv Aerosp Technol, Seoul 08826, South KoreaSeoul Natl Univ, Dept Aerosp Engn, Seoul 08826, South Korea
Jeung, In-Seuck
;
Houwing, A. F. P.
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机构:
Australian Natl Univ, Fac Sci, Dept Phys, GPO Box 4, Canberra, ACT 0200, AustraliaSeoul Natl Univ, Dept Aerosp Engn, Seoul 08826, South Korea
机构:
Lincoln Univ Coll, Fac Engn, Petaling Jaya 47301, MalaysiaLincoln Univ Coll, Fac Engn, Petaling Jaya 47301, Malaysia
Athithan, A. Antony
;
Jeyakumar, S.
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机构:
Lincoln Univ Coll, Fac Engn, Petaling Jaya 47301, Malaysia
Kalasalingam Acad Res & Educ, CFD Ctr, Aeronaut Engn, Krishnankoil 626126, IndiaLincoln Univ Coll, Fac Engn, Petaling Jaya 47301, Malaysia
Jeyakumar, S.
;
Sczygiol, Norbert
论文数: 0引用数: 0
h-index: 0
机构:
Czestochowa Tech Univ, Fac Mech Engn & Comp Sci, PL-42201 Czestochowa, PolandLincoln Univ Coll, Fac Engn, Petaling Jaya 47301, Malaysia
Sczygiol, Norbert
;
Urbanski, Mariusz
论文数: 0引用数: 0
h-index: 0
机构:
Czestochowa Tech Univ, Fac Civil Engn, PL-42201 Czestochowa, PolandLincoln Univ Coll, Fac Engn, Petaling Jaya 47301, Malaysia
Urbanski, Mariusz
;
Hariharasudan, A.
论文数: 0引用数: 0
h-index: 0
机构:
Kalasalingam Acad Res & Educ, Fac English, Krishnankoil 626126, IndiaLincoln Univ Coll, Fac Engn, Petaling Jaya 47301, Malaysia
机构:
Seoul Natl Univ, Dept Aerosp Engn, Seoul 08826, South KoreaSeoul Natl Univ, Dept Aerosp Engn, Seoul 08826, South Korea
Jeong, Eunju
;
O'Byrne, Sean
论文数: 0引用数: 0
h-index: 0
机构:
Univ New South Wales, Australian Def Force Acad, Sch Aerosp & Mech Engn, Canberra, ACT 2600, AustraliaSeoul Natl Univ, Dept Aerosp Engn, Seoul 08826, South Korea
O'Byrne, Sean
;
Jeung, In-Seuck
论文数: 0引用数: 0
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机构:
Seoul Natl Univ, Dept Aerosp Engn, Seoul 08826, South Korea
Seoul Natl Univ, Inst Adv Aerosp Technol, Seoul 08826, South KoreaSeoul Natl Univ, Dept Aerosp Engn, Seoul 08826, South Korea
Jeung, In-Seuck
;
Houwing, A. F. P.
论文数: 0引用数: 0
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机构:
Australian Natl Univ, Fac Sci, Dept Phys, GPO Box 4, Canberra, ACT 0200, AustraliaSeoul Natl Univ, Dept Aerosp Engn, Seoul 08826, South Korea