[go: up one dir, main page]

Ko¨ nig et al., 2004 - Google Patents

Clocking Effects in a 1.5-Stage Axial Turbine: Boundary Layer Behaviour at Midspan

Ko¨ nig et al., 2004

Document ID
10956035070656556298
Author
Ko¨ nig S
Heidecke A
Stoffel B
Fiala A
Engel K
Publication year
Publication venue
Turbo Expo: Power for Land, Sea, and Air

External Links

Snippet

This paper presents an experimental and numerical investigation on the influence of clocking on the boundary layer behaviour of the second stator in a 1.5-stage axial low pressure turbine. Surface mounted hot-film sensors were used to measure the quasi shear …
Continue reading at asmedigitalcollection.asme.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
    • 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
    • Y02EREDUCTION OF GREENHOUSE GASES [GHG] EMISSION, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources

Similar Documents

Publication Publication Date Title
Ye et al. Numerical investigation of blade tip grooving effect on performance and dynamics of an axial flow fan
Haselbach et al. The application of ultra high lift blading in the BR715 LP turbine
Ko¨ nig et al. Clocking Effects in a 1.5-Stage Axial Turbine: Boundary Layer Behaviour at Midspan
Solomon Unsteady boundary layer transition on axial compressor blades
Yang et al. Optimization Design and Experimental Study of Low‐Pressure Axial Fan with Forward‐Skewed Blades
Power et al. Numerical and experimental findings of a highly-loaded aspirated cascade
Yan et al. Aerodynamic design, model test, and CFD analysis for a multistage axial helium compressor
Mistry et al. Experimental investigation of a high aspect ratio, low speed contra-rotating fan stage with complex inflow distortion
Beselt et al. Impact of hub clearance on endwall flow in a highly loaded axial compressor stator
Singh et al. An Aerodynamic Investigation of a High-Pressure Turbine Using Rotor Casing Static Pressure Measurements at Engine Representative Conditions With Different Tip Designs, Tip Gaps, and Inlet Temperature Profiles
Beselt et al. Experimental and numerical investigations of rotating instability phenomenon in an axial compressor stator
Outa et al. An NS simulation of stall cell behavior in a 2-D compressor rotor-stator system at various loads
Mank et al. Secondary flows and fillet radii in a linear turbine cascade
Williams et al. Low pressure ratio transonic fan stall with radial distortion
Gombert et al. Unsteady aerodynamical blade row interaction in a new multistage research turbine: Part 1—experimental investigation
Casartelli et al. Numerical flow analysis in a subsonic vaned radial diffuser with leading edge redesign
Gundy-Burlet et al. Temporally and spatially resolved flow in a two-stage axial compressor: Part 2—Computational assessment
Gottschall et al. The effect of two different endwall-penny concepts for variable stator vanes in a compressor cascade
Nishi et al. Rotor Design Method for a Propeller-Type Wind Turbine that Combines Optimization Method with the Blade Element Momentum Theory
Dai Modelling Considerations for a Transonic Fan
Chana et al. Turbine heat transfer and aerodynamic measurements and predictions for a 1.5 stage configuration
Pullan et al. Improving the performance of a turbine with low aspect ratio stators by aft-loading
Horlock Some recent research in turbo-machinery
Hodson et al. Three-dimensional interactions in the rotor of an axial turbine
Canepa et al. Influence of aerodynamic loading on rotor-stator aerodynamic interaction in a two-stage low pressure research turbine