Application of Boundary Layer Fences and Vortex Generators in Improving Performance of S-Duct Diffusers
Author:
Affiliation:
1. Department of Aerospace Engineering, Indian Institute of Technology, Kanpur-208 016, India
2. Department of Aerospace Engineering, Indian Institute of Technology, Kanpur, India
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/fluidsengineering/article-pdf/124/1/136/5900966/136_1.pdf
Reference17 articles.
1. Guo, R.W., and Seddon, J., 1983, “The Swirl in an S-duct of Typical Air Intake Proportions,” Aeronaut. Q., 34, pp. 99–129.
2. Weng, P.F., and Guo, R.W., 1994, “New Method of Swirl Control in a Diffusing S-duct,” AIAA J., 30, No. 7, Technical Notes, pp. 1918–1919.
3. Taylor, A.M.K.P., Whitelaw, J.H., and Yianeskis, M., 1982, “Curved Ducts with Strong Secondary Motion: Velocity Measurements of Developing Laminar and Turbulent Flow,” ASME J. Fluids Eng., 104, pp. 350–359.
4. McConnaughey, P., Cornelison, J., and Barker, L., “The Prediction of Secondary Flows in Curved S-ducts of Square Cross-Section,” 1989, AIAA Paper 89-0276.
5. Majumdar, B., Singh, S.N., and Agarwal, D.P., 1997, “Flow Characteristics in S-Shaped Diffusing Duct,” International Journal of Turbo and Jet Engines, 14, pp. 45–57.
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