Numerical Simulation of Compressible Flow in a Diffusing S-duct with and without Vortex Generators
Author:
Affiliation:
1. University of Tennessee, Chattanooga
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-2715
Reference22 articles.
1. Computational Investigation of Compressible Flow in a Diffusing S-duct
2. Experimental and Computational Evaluation of Flush-Mounted, S-Duct Inlets
3. A Numerical Investigation of S-Duct Flows with Boundary-Layer Ingestion
4. Demonstration of Sub-system Level Simulations: A Coupled Inlet and Turbofan Stage
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1. Numerical study on adjustment of the main flow field with guide vanes in transition zone for an S-duct;Advances in Mechanical Engineering;2022-02
2. Influence of Propeller Slipstream on the Flow Field of S-Shaped Intake;International Journal of Aerospace Engineering;2021-10-27
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