Numerical study on the placement of vortex generator in a serpentine air intake duct
Author:
Publisher
Springer Science and Business Media LLC
Subject
Multidisciplinary
Link
https://link.springer.com/content/pdf/10.1007/s12046-023-02120-4.pdf
Reference13 articles.
1. Hamstra J W, Miller D N, Truax P P, Anderson B A and Wendt B J 2000 Active inlet flow control technology demonstration The Aeronautical Journal 104(1040): 473–479
2. Wellborn S, Reichert B and Okiishi T 1992 An experimental investigation of the flow in a diffusing S-duct. In: 28th joint propulsion conference and exhibit, p. 3622
3. Chima R, Arend D, Castner R and Slater J 2010 CFD models of a serpentine inlet, fan, and nozzle. In: 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, p. 33
4. Dudek J C 2007 S-Duct inlet. https://www.grc.nasa.gov/ WWW/wind/valid/sduct/sduct02/sduct02.html. Accessed 20 Oct. 2022
5. Patel T, Singh S N and Seshadri V 2005 Characteristics of Y-shaped rectangular diffusing duct at different inflow conditions. Journal of aircraft 42(1): 113–120
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