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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

has been cited by the following article:

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

  AUTHORS: S. M. Prabhu, Abbas Mohadeen

  KEYWORDS: Adiabatic Proces, Friction Efects, Nozzle Modeling, Materialbehavior

  JOURNAL NAME: Materials Sciences and Applications, Vol.2 No.10, October 24, 2011

  ABSTRACT: 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.