Javascript must be enabled to continue!
Effect of Expansion Direction/Area Ratio on Loss Characteristics and Flow Rectification of Curve Diffuser
View through CrossRef
Curve diffuser is frequently used in applications such as HVAC, wind- tunnel, gas turbine cycle, aircraft engine etc. as an adapter to join the conduits of different cross-sectional areas or an ejector to decelerate the flow and raise the static pressure before discharging to the atmosphere. The performance of the curve diffuser is greatly affected by the abrupt expansion and inflection introduced, particularly when a sharp 90o curve diffuser is configured with a high area ratio (AR). Therefore, the paper aims to numerically investigate the effect of the expansion direction of AR=1.2 to 4.0 curve diffuser on loss characteristic and flow rectification. 90o curve diffuser operated at inflow Reynolds Number, Rein=5.934 × 104 to 1.783 × 105 was considered. Results show that pressure recovery improves when the area ratio increases from 1.2 to 2.16 for both 2D expansion (z- direction) and 3D expansion (x- and z- direction). On the other hand, the increase of inflow Reynolds number causes the flow uniformity to drop regardless of the expansion directions. 3D expansion (x- and z- direction) curve diffuser with AR=2.16, operated at Rein=8.163 × 104, is opted as the most optimum, producing the best pressure recovery up to 0.380. Meanwhile, 2D expansion (z-direction) curve diffuser of AR=2.16, , operated at Rein= 5.934 × 104, is chosen to provide the best flow uniformity of 2.330 m/s. 2D expansion (x- direction) should be as best avoided as it provides the worst overall performance of 90o curve diffuser.
Title: Effect of Expansion Direction/Area Ratio on Loss Characteristics and Flow Rectification of Curve Diffuser
Description:
Curve diffuser is frequently used in applications such as HVAC, wind- tunnel, gas turbine cycle, aircraft engine etc.
as an adapter to join the conduits of different cross-sectional areas or an ejector to decelerate the flow and raise the static pressure before discharging to the atmosphere.
The performance of the curve diffuser is greatly affected by the abrupt expansion and inflection introduced, particularly when a sharp 90o curve diffuser is configured with a high area ratio (AR).
Therefore, the paper aims to numerically investigate the effect of the expansion direction of AR=1.
2 to 4.
0 curve diffuser on loss characteristic and flow rectification.
90o curve diffuser operated at inflow Reynolds Number, Rein=5.
934 × 104 to 1.
783 × 105 was considered.
Results show that pressure recovery improves when the area ratio increases from 1.
2 to 2.
16 for both 2D expansion (z- direction) and 3D expansion (x- and z- direction).
On the other hand, the increase of inflow Reynolds number causes the flow uniformity to drop regardless of the expansion directions.
3D expansion (x- and z- direction) curve diffuser with AR=2.
16, operated at Rein=8.
163 × 104, is opted as the most optimum, producing the best pressure recovery up to 0.
380.
Meanwhile, 2D expansion (z-direction) curve diffuser of AR=2.
16, , operated at Rein= 5.
934 × 104, is chosen to provide the best flow uniformity of 2.
330 m/s.
2D expansion (x- direction) should be as best avoided as it provides the worst overall performance of 90o curve diffuser.
Related Results
Effect of Angle of Turn on Loss Characteristics and Flow Rectification of Curve Diffuser
Effect of Angle of Turn on Loss Characteristics and Flow Rectification of Curve Diffuser
Curve diffuser is often used in HVAC and wind tunnel systems to provide pressure recovery and avoid excessive energy loss to the surrounding environment. Performance of curve diffu...
Perancangan diffuser aromaterapi menggunakan metode quality function deployment
Perancangan diffuser aromaterapi menggunakan metode quality function deployment
Diffuser aromaterapi merupakan suatu alat yang bisa mengolah air dengan tetesan cairan aromaterapi. Diffuser aromaterapi dapat digunakan di berbagai tempat seperti ruang keluarga, ...
Effect of Vaned Diffuser on a Small Centrifugal Impeller Performance
Effect of Vaned Diffuser on a Small Centrifugal Impeller Performance
A small transonic centrifugal compressor with 3D vaned diffuser has been developed for a turbine engine by Nanjing University of Aeronautics and Astronautics. The centrifugal impel...
CFD investigation of flow through a centrifugal compressor diffuser with splitter blades
CFD investigation of flow through a centrifugal compressor diffuser with splitter blades
AbstractThe aerodynamic losses in centrifugal compressors are mainly associated with the separated flow on the suction sides of impeller and diffuser vanes. The overall performance...
Numerical Investigation of Diffuser Flow Field and Rotating Stall in a Centrifugal Compressor With Vaned Diffuser
Numerical Investigation of Diffuser Flow Field and Rotating Stall in a Centrifugal Compressor With Vaned Diffuser
The diffuser rotating stall in a centrifugal compressor with vaned diffuser is one of important unsteady flow phenomena, which limits the operating range of the compressor. In this...
Investigation on Clocking Effect of Diffuser in a Multi-Stage Centrifugal Pump
Investigation on Clocking Effect of Diffuser in a Multi-Stage Centrifugal Pump
Abstract
The clocking effect is an important phenomenon in the multi-stage Rotating machinery. In order to master the rules and mechanism of diffuser clocking effect on the...
The Application of PIV in the Study of Impeller-Diffuser Interaction in Centrifugal Fan: Part II — Impeller-Vaned Diffuser Interaction
The Application of PIV in the Study of Impeller-Diffuser Interaction in Centrifugal Fan: Part II — Impeller-Vaned Diffuser Interaction
Abstract
The real flow inside a turbomachinery passage is unsteady and strongly affected by wakes between stator and rotor. The aim of this study was to help our und...
Parameter Optimization of Combustor Dump Diffuser Based on RSM
Parameter Optimization of Combustor Dump Diffuser Based on RSM
Abstract
At present, dump diffuser is basically adopted in the combustion chamber of aeroengine. The total pressure loss in it may account for 30% or even higher in ...

