[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Tabakoff et al., 1976 - Google Patents

Effect of solid particles on turbine performance

Tabakoff et al., 1976

Document ID
10153147070889100059
Author
Tabakoff W
Hosny W
Hamed A
Publication year

External Links

Snippet

A theoretical method was developed for predicting the pressure distribution over a blade in cascade for a compressible flow with solid particles. Experimental results were obtained from a cascade wind tunnel equipped with a solid particle injection system. Good agreement …
Continue reading at asmedigitalcollection.asme.org (other versions)

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
    • 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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system

Similar Documents

Publication Publication Date Title
Tabakoff et al. Effect of solid particles on turbine performance
Kanda et al. Mach 8 testing of a scramjet engine model
Yatsuyanagi et al. Ramjet engine test facility (RJTF) in NAL-KRC, Japan
Tabakoff et al. Effect of suspended solid particles on the properties in cascade flow
Heiser Ejector thrust augmentation
Ott et al. Experimental and numerical study of the time-dependent pressure response of a shock wave oscillating in a nozzle
Lin et al. Effect of inlet air pre-cooling of water injection on compressor performance at high flight Mach
Kim et al. Recovery temperature measurement of underexpanded sonic jets impinging on a flat plate
McArdle Internal characteristics and performance of an aerodynamically controlled, variable-discharge convergent nozzle
CN112555901B (en) Method for improving fuel blending of scramjet by unstable motion of shock wave string
Braun et al. Design and experimental assessment of bladeless turbines for axial inlet supersonic flows
Kurzrock Experimental investigation of supersonic turbine performance
Grannan et al. Small Turbojet Altitude Test Facility with Two Stage Turbocharger Inlet Air Cooling
Jones et al. The rolling moment due to sideslip of triangular, trapezoidal, and related plan forms in supersonic flow
Mitani et al. Flow choking by drag and combustion in supersonic engine testing
Chen et al. Experimental investigation of a solid propellant ducted rocket with a chin type inlet
Hiraiwa et al. Performance variation of scramjet nozzle at various nozzle pressure ratios
DURMUŞ et al. Effect of compression ratio and turbine inlet temperature on turboprop engine performance
Metzger et al. Predicted film cooling near flush slots-Comparison with experiment
Forney et al. Dynamics of particle—shock interactions: part I: similitude
Masuya et al. Performance evaluation of scramjet combustors using kinetic energy and combustion efficiencies
Rodriguez An Experimental Study of Thrust Augmentation with Asymmetrical Nozzle Driven Pulsed Ejector
Ivie et al. Supersonic particle probes: Measurement of internal wall losses
Moffitt et al. Experimental investigation of the partial-admission performance characteristics of a single-stage mach 2 supersonic turbine
Masumoto et al. Experimental study on effect of boundary layer on combustion modes in a supersonic combustor