[go: up one dir, main page]

Dudebout et al., 1998 - Google Patents

Numerical simulation of hypersonic shock-induced combustion ramjets

Dudebout et al., 1998

Document ID
15940116841617926333
Author
Dudebout R
Sislian J
Oppitz R
Publication year
Publication venue
Journal of Propulsion and Power

External Links

Snippet

IT has long been established that the engine cycle of choice for hypersonic air-breathing propulsion is the supersoniccombustion ramjet or scramjet. In this type of engine, to avoid very high temperatures and, consequently, high levels of dissociation of air and combustion …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies
    • Y02T50/67Relevant aircraft propulsion technologies
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60Constructional parts; Details
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K7/00Plants 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
    • F02K7/10Plants 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
    • F02K7/16Composite ram-jet/turbo-jet engines
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • B64G1/402Propellant tanks; Feeding propellants
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78Other construction of jet pipes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/97Rocket nozzles
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02Aircraft characterised by the type or position of power plant

Similar Documents

Publication Publication Date Title
Dudebout et al. Numerical simulation of hypersonic shock-induced combustion ramjets
Waltrup et al. Structure of shock waves in cylindrical ducts
Smart Scramjets
Hank et al. The X-51A scramjet engine flight demonstration program
Curran et al. Scramjet propulsion
Smart How much compression should a scramjet inlet do?
Fry A century of ramjet propulsion technology evolution
Yungster Numerical study of shock-wave/boundary-layer interactions in premixed combustible gases
Sislian et al. Propulsive performance of hypersonic oblique detonation wave and shock-induced combustion ramjets
Yi et al. Effect of nozzle shapes on the performance of continuously-rotating detonation engine
Javaid et al. Airframe-propulsion integration methodology for waverider-derived hypersonic cruise aircraft design concepts
Bussing et al. Pulse detonation engine preliminary design considerations
White et al. Evolution and application of CFD techniques for scramjet engine analysis
Lee et al. Design and analysis of an ideal scramjet flowpath
Yungster et al. Multiple-cycle simulation of a pulse detonation engine ejector
Olds et al. SCCREAM: a conceptual rocket-based combined-cycle engine performance analysis tool
Markell Exergy methods for the generic analysis and optimization of hypersonic vehicle concepts
Cheng Hypersonic propulsion
Kodera et al. Numerical analysis of transient phenomena to ramjet mode in a RBCC combustor
Haws et al. Computational investigation of a method to compress air fluidically in supersonic inlets
Javaid et al. Thrust-matching requirements for the conceptual design of hypersonic waverider vehicles
Bezgin et al. Some estimations of a possibility to utilize shock-induced combustion in propulsion systems
Kouchi et al. Performance of a RBCC combustor operating in ramjet mode
Bouchez et al. Airbreathing space launcher interest of a fully variable geometry propulsion system-Status 1999
Savino et al. Numerical analysis of supersonic combustion ramjet with upstream fuel injection