Characterization of Unsteady Flow Structures Around Tandem Cylinders for Component Interaction Studies in Airframe Noise
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-2812
Reference35 articles.
1. 2Li,F.,Khorrami,M.R.,andMalik,M.R."UnsteadySimulationofaLanding-GearFlowField,"AIAA-2002-2411,2002.
2. 3Lopes, L. V., Brentner, K. S., Morris, P. J., Lilley, G. M. and Lockard, D. P. "Complex Landing Gear Noise Prediction UsingaSimpleToolkit,"AIAA-2005-1202, 2005.
3. Nonintrusive measurements of the boundary layer developing on a single and two circular cylinders
4. Fluctuating fluid forces acting on two circular cylinders in a tandem arrangement at a subcritical Reynolds number
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