Share This Article:

Analysis of Material Behavior for Friction in a Nozzle for Turbomachinery and High Speed Vehicles

Abstract Full-Text HTML Download Download as PDF (Size:665KB) PP. 1485-1490
DOI: 10.4236/msa.2011.210200    4,486 Downloads   7,884 Views  


Shock-induced separation of turbulent boundary layers represents a long-studied problem in compressible flow, bearing, for example, on applications in high speed aerodynamics, rocketry, wind tunnel design, and turbomachinery. Experimental investigations have generally sought to expose essential physics using geometrically simple configurations.

Conflicts of Interest

The authors declare no conflicts of interest.

Cite this paper

S. Prabhu and A. Mohadeen, "Analysis of Material Behavior for Friction in a Nozzle for Turbomachinery and High Speed Vehicles," Materials Sciences and Applications, Vol. 2 No. 10, 2011, pp. 1485-1490. doi: 10.4236/msa.2011.210200.


[1] G. Settles, “Details of a Shock-Separated Turbulent Bound- ary Layer at a Compression Corner,” AIAA Journal, Vol. 14, No. 12, 1976, pp. 1709-1715. doi:10.2514/3.61513
[2] D. R. Chapman, D. M. Kuehn and H. K. Larson, “Investigation of Separated Flows in Supersonic and Subsonic Streams with Emphasis on the Effect of Transition,” NACA Report 1356, 1958.
[3] M. E. Erengil and D. S. Dolling, “Correlation of Separation Shock Motion with Pressure Fluctuations in the Incoming Boundary Layer,” AIAA Journal, Vol. 29, No. 11, 1990, pp. 1868-1877. doi:10.2514/3.10812
[4] D. S. Dolling and L. Brusniak, “Separation Shock Motion in Fin, Cylinder, and Compression Ramp-Induced Turbulent Interactions,” AIAA Journal, Vol. 27, No. 6, 1988, pp. 734-742. doi:10.2514/3.10173
[5] J. Ackeret, F. Feldman and N. Rott, “Investigations of Compression Shocks and Boundary Layers in Gases Moving at High Speed,” NACA TM No. 1113, 1947.
[6] D. S. Dolling and D. R. Smith, “Separation Shock Dynamics in Mach 5 Turbulent Interactions Induced by Cylinders,” AIAA Journal, Vol. 27, No. 12, 1989, pp. 1698-1706. doi:10.2514/3.10323
[7] R. A. Gramann and D. S. Dolling, “Detection of Turbulent Boundary-Layer Separation Using Fluctuating Wall Pressure Signals,” AIAA Journal, Vol. 28, No. 6, 1989, pp. 1052-1056. doi:10.2514/3.25164
[8] J. Ostlund, “Flow Processes in Rocket Engine Nozzles with Focus on Flow-Separation and Side-Loads,” Licentiate Thesis, Royal Inst. of Technology, Stockholm, TRITA-MEK, Technique Report, 2002, p. 1112.

comments powered by Disqus

Copyright © 2019 by authors and Scientific Research Publishing Inc.

Creative Commons License

This work and the related PDF file are licensed under a Creative Commons Attribution 4.0 International License.