Nothing Special   »   [go: up one dir, main page]

Hamed, 1982 - Google Patents

Particle dynamics of inlet flowfields with swirling vanes

Hamed, 1982

Document ID
434824925084430396
Author
Hamed A
Publication year
Publication venue
Journal of Aircraft

External Links

Snippet

MANY gas turbine engines operate in environments where the ingestion of solid particles is inevitable. In aircraft and naval installations the particles encountered can be sand, dust, or salt. Solid particles are also ingested by gas turbine engines in ground vehicles, auxiliary …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or anti-vibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/141Shape, i.e. outer, aerodynamic form
    • 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
    • Y02T50/671Measures to reduce the propulsor weight
    • 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
    • Y02T50/673Improving the rotor blades aerodynamic
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry

Similar Documents

Publication Publication Date Title
Chima Explicit multigrid algorithm for quasi-three-dimensional viscous flows in turbomachinery
Hah et al. Secondary flows and vortex motion in a high-efficiency backswept impeller at design and off-design conditions
Hamed Particle dynamics of inlet flowfields with swirling vanes
Beacher et al. Improved particle trajectory calculations through turbomachinery affected by coal ash particles
Barker et al. Influence of compressor exit conditions on combustor annular diffusers part II: flow redistribution
Hsiao et al. Actuator duct model of turbomachinery components for powered-nacelle Navier-Stokes calculations
Morchoisne Pseudo-spectral space-time calculations of incompressible viscous flows
Elfeki et al. Erosion study of radial flow compressor with splitters
Hamed Effect of particle characteristics on trajectories and blade impact patterns
CHIMA Development of an explicit multigrid algorithm for quasi-three-dimensional viscous flows in turbomachinery
Hamed Solid particle dynamic behavior through twisted blade rows
Hall et al. Calculation of three-dimensional unsteady flows in turbomachinery using the linearized harmonic euler equations
Knapke et al. Time accurate simulations of a counter-rotating aspirated compressor
ANDERSON et al. Application of computational fluid dynamics to the study of vortex flow control for the management of inlet distortion
ANDERSON The aerodynamic characteristics of vortex ingestion for the F/A-18 inlet duct
Zedan et al. Viscous flow analysis of advanced particle separators
Tabakoff et al. The dynamics of suspended solid particles in a two stage gas turbine
Surampudi et al. Unsteady transonic flow over cascade blades
Zamiri et al. Influence of the inclined leading edge diffuser vanes on the aerodynamic performance of a transonic centrifugal compressor
Stein et al. Numerical analysis of stall and surge in a high-speed centrifugal compressor
Copenhaver et al. The effect of tip clearance on a swept transonic compressor rotor
Enikeev et al. Analysis of the particle motion dynamics in the compressor to accompany erosion resistance testing of blade material
Briley et al. Computation of flow past a turbine blade with and without tip clearance
Lagha et al. Body force modeling of the fan stage of a windmilling turbofan
Clevenger et al. Dust particle trajectories in aircraft radial turbines