Zhao et al., 2022 - Google Patents
Experimental investigation of combustion mode transitions on solid rocket scramjet combustorZhao et al., 2022
- Document ID
- 2869333283597734483
- Author
- Zhao L
- Xia Z
- Ma L
- Chen B
- Feng Y
- Yang P
- Li C
- Duan Y
- Publication year
- Publication venue
- Aerospace Science and Technology
External Links
Snippet
Based on the design configuration of a solid scramjet combustor, the direct-connect experimented investigation of combustion modes transition was carried out, simulating inflow conditions of Mach number 6.0 and flight altitude 25 km. It is the first experimental …
- 238000002485 combustion reaction 0 title abstract description 120
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
- F02K7/16—Composite ram-jet/turbo-jet engines
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies
- Y02T50/67—Relevant aircraft propulsion technologies
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/30—Use of alternative fuels
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/02—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
- F02K3/105—Heating the by-pass flow
- F02K3/11—Heating the by-pass flow by means of burners or combustion chambers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Wang et al. | Analysis of the maximum flight Mach number of hydrocarbon-fueled scramjet engines under the flight cruising constraint and the combustor cooling requirement | |
Yu et al. | Investigation of kerosene combustion characteristics with pilot hydrogen in model supersonic combustors | |
Frolov et al. | Three-dimensional numerical simulation of operation process in rotating detonation engine | |
Tian et al. | Numerical study on effect of air throttling on combustion mode formation and transition in a dual-mode scramjet combustor | |
Shi et al. | Experimental study on ejector-to-ramjet mode transition in a divergent kerosene-fueled RBCC combustor with low total temperature inflow | |
Dubrovskii et al. | Three-dimensional numerical simulation of the characteristics of a ramjet power plant with a continuous-detonation combustor in supersonic flight | |
Zhang et al. | Effect of Mach number and equivalence ratio on the pressure rising variation during combustion mode transition in a dual-mode combustor | |
Rubins et al. | Review of shock-induced supersonic combustion research and hypersonic applications | |
Zhao et al. | Experimental investigation of combustion mode transitions on solid rocket scramjet combustor | |
Meng et al. | Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration | |
Ye et al. | Investigation of RBCC performance improvements based on a variable geometry ramjet combustor | |
Xue et al. | Experimental study on combustion modes of a liquid kerosene fueled RBCC combustor | |
Yan et al. | Experimental investigations on pulse detonation rocket engine with various injectors and nozzles | |
Yang et al. | Experimental study on the influence of the injection structure on solid scramjet performance | |
Li et al. | Fuel reactivity controlled self-starting and propulsion performance of a scramjet: a model investigation | |
Yonggang et al. | Influence of lobe geometry on mixing and heat release characteristics of solid fuel rocket scramjet combustor | |
Hu et al. | Combustion stabilization based on a center flame strut in a liquid kerosene fueled supersonic combustor | |
Wang et al. | Research on the operating boundary of the dual mode scramjet with a constant area combustor through thermodynamic cycle analysis | |
Fang et al. | Experimental and numerical investigation of an embedded rocket ramjet combustor | |
Dai et al. | Secondary fuel jet strategies on mixing enhancement performance of rocket-based combined cycle engine | |
Wang et al. | Back-propagation suppression study based on intake configuration optimization for an air-breathing pulse detonation engine | |
Ogorodnikov et al. | Russian research on experimental hydrogen-fueled dual-mode scramjet: conception and preflight tests | |
Tomioka et al. | Supersonic combustion with supersonic injection through diamond-shaped orifices | |
Li et al. | Performance analysis of an ethylene-fueled scramjet with adjustable finite-rate chemistry | |
Guoskov et al. | Numerical research of gaseous fuel preinjection in hypersonic three-dimensional inlet |