Effect of Fan on Inlet Distortion: Mixed-Fidelity Approach
Author:
Affiliation:
1. University of Cambridge, Cambridge, England CB2 1PZ, United Kingdom
2. Zhejiang University, Hangzhou 310007, People’s Republic of China
Funder
Engineering and Physical Sciences Research Council
Chinese Scholarship Council
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J056858
Reference39 articles.
1. Fan–Intake Interaction Under High Incidence
2. A Study of Fan-Distortion Interaction Within the NASA Rotor 67 Transonic Stage
3. Unsteady CFD Simulation of Transonic Axial Compressor Stages with Distorted Inflow
4. Intake Aerodynamics, Second Edition
5. Turbulence Modeling for Flows Around Convex Features
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