Linked Data Explorerhttp://worldcat.org/entity/work/id/3536788
Performance of a tandem-rotor/tandem-stator conical-flow compressor designed for a pressure ratio of 3
A conical-flow compressor stage with a large radius change through the rotor was tested at three values of rotor tip clearance. The stage had a tandem rotor and a tandem stator. Peak efficiency at design speed was 0.774 at a pressure ratio of 2.613. The rotor was tested without the stator, and detailed survey data were obtained for each rotor blade row. Overall peak rotor efficiency was 0.871 at a pressure ratio of 2.952. (Author).
Open All Close All
http://schema.org/about
- http://experiment.worldcat.org/entity/work/data/3536788#Topic/compression_ratio
- http://experiment.worldcat.org/entity/work/data/3536788#Topic/tables_data
- http://experiment.worldcat.org/entity/work/data/3536788#Topic/equations
- http://id.loc.gov/authorities/subjects/sh85115506
- http://id.worldcat.org/fast/1100674
- http://id.loc.gov/authorities/subjects/sh85138741
- http://experiment.worldcat.org/entity/work/data/3536788#Topic/aerodynamic_characteristics
- http://id.loc.gov/authorities/subjects/sh85029444
- http://experiment.worldcat.org/entity/work/data/3536788#Topic/performance_tests
- http://experiment.worldcat.org/entity/work/data/3536788#Topic/radius_measure
- http://id.worldcat.org/fast/1159204
- http://experiment.worldcat.org/entity/work/data/3536788#Topic/compressor_stators
- http://experiment.worldcat.org/entity/work/data/3536788#Topic/pressure_measurement
- http://experiment.worldcat.org/entity/work/data/3536788#Topic/performance_engineering
- http://experiment.worldcat.org/entity/work/data/3536788#Topic/compressor_rotors
- http://experiment.worldcat.org/entity/work/data/3536788#Topic/hydraulic_and_pneumatic_equipment
- http://id.worldcat.org/fast/871908
- http://experiment.worldcat.org/entity/work/data/3536788#Topic/high_pressure_compressors
- http://experiment.worldcat.org/entity/work/data/3536788#Topic/axial_flow_compressor_blades
- http://experiment.worldcat.org/entity/work/data/3536788#Topic/gas_turbines
http://schema.org/contributor
- http://worldcat.org/entity/person/id/2632082351
- http://worldcat.org/entity/person/id/2631924322
- http://viaf.org/viaf/126233085
- http://id.loc.gov/authorities/names/n79039093
- http://experiment.worldcat.org/entity/work/data/3536788#Organization/national_aeronautics_and_space_administration_cleveland_oh_lewis_research_center
- http://viaf.org/viaf/155061179
- http://viaf.org/viaf/157091911
- http://id.loc.gov/authorities/names/n78091122
- http://worldcat.org/entity/person/id/2629333316
- http://id.loc.gov/authorities/names/n80126316
http://schema.org/description
- "A conical-flow compressor stage with a large radius change through the rotor was tested at three values of rotor tip clearance. The stage had a tandem rotor and a tandem stator. Peak efficiency at design speed was 0.774 at a pressure ratio of 2.613. The rotor was tested without the stator, and detailed survey data were obtained for each rotor blade row. Overall peak rotor efficiency was 0.871 at a pressure ratio of 2.952. (Author)."@en
http://schema.org/name
- "Performance of a tandem-rotor/tandem-stator conical-flow compressor designed for a pressure ratio of 3"
- "Performance of a tandem-rotor/tandem-stator conical-flow compressor designed for a pressure ratio of 3"@en
- "Performance of a Tandem-Rotor/Tandem-Stator Conical-Flow Compressor Designed for a Pressure Ratio of 3"@en