Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 892
Book Description
Applied Mechanics Reviews
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 892
Book Description
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 892
Book Description
Effects of Tip Clearance on Overall Performance of Transonic Fan Stage with and Without Casing Treatment
Author: Royce D. Moore
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
Book Description
Effect of Casing Treatment on Performance of a Two-stage High-pressure-ratio Fan
Author: Donald C. Urasek
Publisher:
ISBN:
Category : Fans (Machinery)
Languages : en
Pages : 76
Book Description
Publisher:
ISBN:
Category : Fans (Machinery)
Languages : en
Pages : 76
Book Description
Fan Performance from Duct Rake Instrumentation on a 1. 294 Pressure Ratio, 725 Ft/sec Tip Speed Turbofan Simulator Using Vaned Passage Casing Treatment
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781720522300
Category :
Languages : en
Pages : 64
Book Description
A 1.294 pressure ratio, 725 ft/sec tip speed, variable pitch low noise fan was designed and tested in the NASA Glenn 9- by 15-foot Wind Tunnel. The design included a casing treatment that used recirculation to extend the fan stall line and provide an acceptable operating range. Overall aerodynamic experimental results are presented for this low tip speed, low noise fan without casing treatment as well as using several variants of the casing treatment that moved the air extraction and insertion axial locations. Measurements were made to assess effects on performance, operability, and noise. An unusual instability was discovered near the design operating line and is documented in the fan operating range. Measurements were made to compare stall margin improvements as well as measure the performance impact of the casing treatments. Experimental results in the presence of simulated inlet distortion, via screens, are presented for the baseline and recirculation casing treatment configurations. Estimates are made for the quantity of recirculation weight flow based on limited instrumentation in the recirculation system along with discussion of results and conclusionsFite, E. BrianGlenn Research CenterTURBOFANS; DISTORTION; DUCTS; EXTRACTION; AERODYNAMICS; LOW NOISE; FAN BLADES; PRESSURE RATIO; WIND TUNNELS; POSITION (LOCATION); TIP SPEED; SIMULATORS
Publisher: Createspace Independent Publishing Platform
ISBN: 9781720522300
Category :
Languages : en
Pages : 64
Book Description
A 1.294 pressure ratio, 725 ft/sec tip speed, variable pitch low noise fan was designed and tested in the NASA Glenn 9- by 15-foot Wind Tunnel. The design included a casing treatment that used recirculation to extend the fan stall line and provide an acceptable operating range. Overall aerodynamic experimental results are presented for this low tip speed, low noise fan without casing treatment as well as using several variants of the casing treatment that moved the air extraction and insertion axial locations. Measurements were made to assess effects on performance, operability, and noise. An unusual instability was discovered near the design operating line and is documented in the fan operating range. Measurements were made to compare stall margin improvements as well as measure the performance impact of the casing treatments. Experimental results in the presence of simulated inlet distortion, via screens, are presented for the baseline and recirculation casing treatment configurations. Estimates are made for the quantity of recirculation weight flow based on limited instrumentation in the recirculation system along with discussion of results and conclusionsFite, E. BrianGlenn Research CenterTURBOFANS; DISTORTION; DUCTS; EXTRACTION; AERODYNAMICS; LOW NOISE; FAN BLADES; PRESSURE RATIO; WIND TUNNELS; POSITION (LOCATION); TIP SPEED; SIMULATORS
Government Reports Annual Index
Author:
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 1048
Book Description
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 1048
Book Description
Detailed Flow Measurements in Casing Boundary Layer of 427-meter-per-second-tip-speed Two-stage Fan with Casing Treatment
Author: William T. Gorrell
Publisher:
ISBN:
Category : Impellers
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Impellers
Languages : en
Pages : 44
Book Description
Performance of a 1.57-pressure-ratio Transonic Fan Stage with a Screen-induced 90 Circumferential Inlet Flow Distortion
Author: Nelson L. Sanger
Publisher:
ISBN:
Category :
Languages : en
Pages : 74
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 74
Book Description
Aerodynamic Performance of a 1.35-pressure-ratio Axial-flow Fan Stage
Author: Walter Martin Osborn
Publisher:
ISBN:
Category : Fans (Machinery)
Languages : en
Pages : 114
Book Description
Publisher:
ISBN:
Category : Fans (Machinery)
Languages : en
Pages : 114
Book Description
Government Reports Announcements & Index
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1058
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1058
Book Description
Aerodynamic Performance of Axial-flow Fan Stage Operated at Nine Inlet Guide Vane Angles
Author: Royce D. Moore
Publisher:
ISBN:
Category : Fans (Machinery)
Languages : en
Pages : 52
Book Description
Publisher:
ISBN:
Category : Fans (Machinery)
Languages : en
Pages : 52
Book Description