Numerical investigation of total temperature distortion problem in a multistage fan based on body force approach
Author:
Affiliation:
1. College of Energy and Power Engineering , Nanjing University of Aeronautics and Astronautics, Jiangsu Province Key Laboratory of Aerospace Power Systems , Nanjing , Jiangsu , China
Abstract
Funder
National Science and Technology Major Project
Publisher
Walter de Gruyter GmbH
Subject
Aerospace Engineering
Link
https://www.degruyter.com/document/doi/10.1515/tjeng-2020-0035/pdf
Reference28 articles.
1. Society of Automotive Engineers. Assessment of the inlet/engine total temperature distortion problem. Aerospace Information Report No 2017. AIR5867.
2. Fidalgo, VJ, Hall, CA, Colin, Y. A study of fan-distortion interaction within the NASA Rotor 67 transonic stage. J Turbomach 2012;134: 051011. https://doi.org/10.1115/1.4003850.
3. Peterson, MW, Gorrell, SE, List, MG, Custer, C. Implementation of fourier methods in CFD to analyze distortion transfer and generation through a transonic fan. AIAA Paper No. 2016-4746.; 2016.
4. Peterson, MW, Gorrell, SE, List, MG. Fourier descriptors for improved analysis of distortion transfer and generation. ASME Paper No. GT2017-65031.; 2017.
5. Soderquist, DR, Gorrell, SE, List, MG. Radial variation in distortion transfer and generation through a highly loaded fan stage. ASME Paper No. GT2018-77221.; 2018.
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