Tomioka et al., 2021 - Google Patents
Sea-level static tests of rocket–ramjet combined cycle engine modelTomioka et al., 2021
View PDF- Document ID
- 479371643625067721
- Author
- Tomioka S
- Takegoshi M
- Kochi T
- Kato K
- Saito T
- Tani K
- Publication year
- Publication venue
- Journal of Propulsion and Power
External Links
Snippet
A rocket–ramjet combined cycle engine model, embedding twin rocket chambers driven with gaseous hydrogen and oxygen on the top wall side of a scramjet flowpath, was tested in its ejector-mode operation under sea-level static conditions. Gaseous hydrogen was also …
- 230000003068 static 0 title abstract description 23
Classifications
-
- 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
-
- 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
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/78—Other construction of jet pipes
- F02K1/82—Jet pipe walls, e.g. liners
-
- 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
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/38—Introducing air inside the 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
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/46—Nozzles having means for adding air to the jet or for augmenting the mixing region between the jet and the ambient air, e.g. for silencing
-
- 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
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Tomioka et al. | Sea-level static tests of rocket–ramjet combined cycle engine model | |
Spaid et al. | A study of the interaction of gaseous jets from transverse slots with supersonic external flows. | |
Santiago et al. | Velocity measurements of a jet injected into a supersonic crossflow | |
Waltrup et al. | Structure of shock waves in cylindrical ducts | |
Smart | How much compression should a scramjet inlet do? | |
Masumoto et al. | Experimental study on combustion modes in a supersonic combustor | |
Turner et al. | Mode change characteristics of a three-dimensional scramjet at Mach 8 | |
Barth et al. | Tailored fuel injection for performance enhancement in a Mach 12 scramjet engine | |
Choubey et al. | Numerical studies on the performance of scramjet combustor with alternating wedge-shaped strut injector | |
Yang et al. | Maximum thrust for the rocket-ejector mode of the hydrogen fueled rocket-based combined cycle engine | |
Etele et al. | Experimental investigation of an alternative rocket configuration for rocket-based combined cycle engines | |
Peng et al. | Effect of coolant inlet conditions on supersonic film cooling | |
Smart | Scramjet inlets | |
Capra et al. | Porous versus porthole fuel injection in a radical farming scramjet: numerical analysis | |
Marshall et al. | Critical issues in TBCC modeling | |
Dai et al. | Secondary fuel jet strategies on mixing enhancement performance of rocket-based combined cycle engine | |
Suneetha et al. | Implication of self-throttling on combustion performance in a strut-based scramjet combustor | |
Wang et al. | Effect of thermal choking on ejection process in a rocket-based combined cycle engine | |
Kouchi et al. | Supersonic combustion using a stinger-shaped fuel injector | |
Etele et al. | Experiments with ejector rocket entrainment | |
Srinivasan et al. | Supersonic combustion of a scramjet engine using hydrogen fuel in shock tunnel | |
Tomioka et al. | Performance of a rocket-ramjet combined-cycle engine model in ejector mode operation | |
Takahashi et al. | Numerical study on combustor flow-path design for a scramjet flight experiment | |
Bricalli et al. | Numerical investigation into the combustion behavior of an inlet-fueled thermal-compression-like scramjet | |
Araki et al. | Acoustic Simulation of Hot Jets Issuing from a Rectangular Hypersonic Nozzle |