THE EFFECTS OF LEAN AND SWEEP ON TRANSONIC FAN PERFORMANCE: A COMPUTATIONAL STUDY

The aerodynamics of transonic fans is discussed with emphasis on the use of threedimensional design techniques, such as blade sweep and lean, to improve their performance. In order to study the interaction of these 3D features with the shock pattern a series of five different designs is produced an...

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Main Author: JOHN D. DENTON
Format: Article
Language:English
Published: Gdańsk University of Technology 2002-01-01
Series:TASK Quarterly
Subjects:
Online Access:https://journal.mostwiedzy.pl/TASKQuarterly/article/view/2258
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author JOHN D. DENTON
author_facet JOHN D. DENTON
author_sort JOHN D. DENTON
collection DOAJ
description The aerodynamics of transonic fans is discussed with emphasis on the use of threedimensional design techniques, such as blade sweep and lean, to improve their performance. In order to study the interaction of these 3D features with the shock pattern a series of five different designs is produced and analysed by CFD. It is found that the 3D features have remarkably little effect on the shock pattern near the tip where the shock must remain perpendicular to the casing. Lower down the blade significant shock sweep, and hence reduced shock loss, can be induced by 3D design but this is usually at the expense of reduced stall margin and increased loss elsewhere along the blade span. Overall, very little change in efficiency is produced by blade sweep or lean. However, forwards lean of the rotor does produce a small increase in mass flow. Radial migration of the boundary fluid on the suction surface behind the shock is shown to play a large part in the aerodynamics near the blade tip.
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spelling doaj.art-f1b92c2f70d44a9ca9ffd1cee9b586b52022-12-22T00:23:12ZengGdańsk University of TechnologyTASK Quarterly1428-63942002-01-0161THE EFFECTS OF LEAN AND SWEEP ON TRANSONIC FAN PERFORMANCE: A COMPUTATIONAL STUDYJOHN D. DENTON0Whittle Laboratory, Cambridge University Engineering Department The aerodynamics of transonic fans is discussed with emphasis on the use of threedimensional design techniques, such as blade sweep and lean, to improve their performance. In order to study the interaction of these 3D features with the shock pattern a series of five different designs is produced and analysed by CFD. It is found that the 3D features have remarkably little effect on the shock pattern near the tip where the shock must remain perpendicular to the casing. Lower down the blade significant shock sweep, and hence reduced shock loss, can be induced by 3D design but this is usually at the expense of reduced stall margin and increased loss elsewhere along the blade span. Overall, very little change in efficiency is produced by blade sweep or lean. However, forwards lean of the rotor does produce a small increase in mass flow. Radial migration of the boundary fluid on the suction surface behind the shock is shown to play a large part in the aerodynamics near the blade tip. https://journal.mostwiedzy.pl/TASKQuarterly/article/view/2258transonic fantransonic compressorthree-dimensional flowshock wavesCFD
spellingShingle JOHN D. DENTON
THE EFFECTS OF LEAN AND SWEEP ON TRANSONIC FAN PERFORMANCE: A COMPUTATIONAL STUDY
TASK Quarterly
transonic fan
transonic compressor
three-dimensional flow
shock waves
CFD
title THE EFFECTS OF LEAN AND SWEEP ON TRANSONIC FAN PERFORMANCE: A COMPUTATIONAL STUDY
title_full THE EFFECTS OF LEAN AND SWEEP ON TRANSONIC FAN PERFORMANCE: A COMPUTATIONAL STUDY
title_fullStr THE EFFECTS OF LEAN AND SWEEP ON TRANSONIC FAN PERFORMANCE: A COMPUTATIONAL STUDY
title_full_unstemmed THE EFFECTS OF LEAN AND SWEEP ON TRANSONIC FAN PERFORMANCE: A COMPUTATIONAL STUDY
title_short THE EFFECTS OF LEAN AND SWEEP ON TRANSONIC FAN PERFORMANCE: A COMPUTATIONAL STUDY
title_sort effects of lean and sweep on transonic fan performance a computational study
topic transonic fan
transonic compressor
three-dimensional flow
shock waves
CFD
url https://journal.mostwiedzy.pl/TASKQuarterly/article/view/2258
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