Numerical Simulations and Design Optimization of Compressor Cascade Flow Using One Equation and Wray-Agarwal Turbulence Model-Reference-Cited by-同舟云学术

Numerical Simulations and Design Optimization of Compressor Cascade Flow Using One Equation and Wray-Agarwal Turbulence Model

Published:2022-09-14 Issue:8 Volume:36 Page:705-718
ISSN:1061-8562
Container-title:International Journal of Computational Fluid Dynamics
language:en
Short-container-title:International Journal of Computational Fluid Dynamics

Author:

Li Zhihui¹,Agarwal Ramesh K.²

Affiliation:

1. Department of Aeronautics, Imperial College London, London, UK

2. McKelvey School of Engineering, Washington University in St. Louis, St. Louis, MO, USA

Funder

H2020 Marie Skłodowska-Curie Actions

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,Energy Engineering and Power Technology,Condensed Matter Physics,Aerospace Engineering,Computational Mechanics

Link

https://www.tandfonline.com/doi/pdf/10.1080/10618562.2023.2187050

Reference26 articles.

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2. Chen, J., and D. Whitfield. 1993. “Navier-Stokes Calculations for the Unsteady Flowfield of Turbomachinery.” American Institute of Aeronautics and Astronautics (AIAA) Paper, AIAA-93-0676.

3. A zero-equation turbulence model for indoor airflow simulation

4. Dawes, W. N. 1988. “Development of a 3d Navier Stokes solver for application to all types of turbomachinery,” American Society of Mechanical Engineers (ASME) Paper, 88-GT-70.

5. Denton, J. D. 1975. “A Time Marching Method for Two- and Three- Dimensional Blade to Blade Flows,” Aeronautical Research Council Reports and Memoranda, Report No. ARC/R&M-3775.

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