Venkatakrishnan, L and Suriyanarayanan, P and Mathur, NB (2007) BOS density measurements in afterbody flows with shock13; and jet effects AIAA 2007-4223. In: 37th AIAA Fluid Dynamics Conference and Exhibit, 25-28 Jun 2007, Miami, FL..Full text not available from this repository.
The Background Oriented Schlieren technique has been applied to determine the density13; field in an oblique shock-separated turbulent boundary flow. Measurements were made for13; two cases, namely, with/without jet flow at flow at the base. Both instantaneous and time-averaged13; density field have been obtained x2013; these results show certain upstream features of13; interest including shock excursions. The mean density field is discussed along with13; conventional Schlieren flow visualization. The study involving shock boundary interaction,13; movement of freestream shock over the afterbody in the presence of a jet plume provides13; understanding of flow physics in a flow regime where whole field velocity measurements are13; extremely difficult.
|Item Type:||Conference or Workshop Item (Paper)|
|Uncontrolled Keywords:||Jet effects;Turbulent boundary flow;Jet plume|
|Subjects:||AERONAUTICS > Aeronautics (General)|
|Division/Department:||Experimental Aerodynamics Division, Experimental Aerodynamics Division, Experimental Aerodynamics Division|
|Depositing User:||Ms. Alphones Mary|
|Date Deposited:||05 Feb 2010|
|Last Modified:||24 May 2010 09:57|
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