Design optimization of a vane type pre-swirl nozzle-Reference-Cited by-同舟云学术

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Design optimization of a vane type pre-swirl nozzle

Published:2021-01-01 Issue:1 Volume:15 Page:164-179
ISSN:1994-2060
Container-title:Engineering Applications of Computational Fluid Mechanics
language:en
Short-container-title:Engineering Applications of Computational Fluid Mechanics

Author:

Lee Jungsoo¹,Lee Hyungyu¹,Park Hyunwoo¹,Cho GeonHwan²,Kim Donghwa³,Cho Jinsoo¹

Affiliation:

1. Department of Mechanical Engineering, Hanyang University, Seoul, Republic of Korea

2. Gas Turbine System Integration Team, Doosan Heavy Industries & Construction, Changwon, Republic of Korea

3. 4th R&D Institute, Agency for Defence Development, Daegeon, Republic of Korea

Funder

Korea Institute of Energy Technology Evaluation and Planning

Ministry of Trade, Industry & Energy

Publisher

Informa UK Limited

Subject

Modeling and Simulation,General Computer Science

Link

https://www.tandfonline.com/doi/pdf/10.1080/19942060.2020.1847199

Reference26 articles.

1. Investigation Into the Computational Analysis of Direct-Transfer Pre-Swirl Systems for Gas Turbine Cooling

2. Measurement and Analysis of Aerodynamic and Thermodynamic Losses in Pre-Swirl System Arrangements

3. Automatic Optimization of Preswirl Nozzle Design

4. Numerical Characterization of Flow and Heat Transfer in Preswirl Systems

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1. Transient response and volume model of steam cooling in a rotor–stator disk cavity of gas turbines;Thermal Science and Engineering Progress;2024-08

2. Cooperative Optimization of Pre-swirl Nozzles and Receiver Holes in a Radial Pre-swirl System Using an ANN-PSO Approach;Journal of Applied Fluid Mechanics;2024-06-01

3. Optimization of a nozzle vane of gas turbine pre-swirl system;Journal of Mechanical Science and Technology;2024-06

4. Prediction and Optimization of Heat Transfer Performance of Premixed Methane Impinging Flame Jet Using the Kriging Model and Genetic Algorithm;Applied Sciences;2024-04-27

5. Experimental and Numerical Investigation of a Novel Vortex Reducer in a Co-Rotating Cavity of Aeroengines;Aerospace;2024-03-13

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