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Interaction of a line vortex with a round parachute canopy
Authors:H. Johari  A. Levshin
Affiliation:1. Department of Mechanical Engineering, California State University, Northridge, CA 91330, USA;2. Department of Mechanical Engineering, Worcester Polytechnic Institute, Worcester, MA 01609, USA;1. GeM, École centrale de Nantes, 1, rue de la Noë, 44321 Nantes, France;2. I3A, Universidad de Zaragoza, Maria de Luna 3, 50018 Zaragoza, Spain;3. University of Lyon, ENISE, LTDS, UMR 5513 CNRS, 58, rue Jean-Parot, 42023 Saint-Étienne cedex 2, France;1. Dept. of Mechanical & Aerospace Engineering, Naval Postgraduate School, Monterey, CA 93943, USA;2. Dept. of Ocean Engineering, US Naval Academy, Annapolis, MD 21402, USA;1. Key Laboratory of Aircraft Environment Control and Life Support, MIIT, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;2. College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;3. Beijing Institute of Space Mechanics & Electricity, Beijing 100094, China
Abstract:The interaction of a rectilinear vortex with an inflated round parachute canopy model was studied experimentally in a water tunnel where the vortex core was aligned with the axis of the canopy. Three different canopy diameters were used, and the canopy model was attached to a streamlined forebody. Dye flow visualization indicated that vortex breakdown was present when the core trajectory was within the canopy opening. Vortex breakdown occurred about one to two canopy diameters upstream of the canopy opening. The vortex core completely disintegrated when it interacted with the forebody near the canopy centerline. The vortex breakdown and disintegration caused unsteady, asymmetric deformations on the canopy surface. A reduction in the time-averaged drag and an increase in the fluctuating drag was observed when the vortex core was within the canopy opening. The disintegration of the vortex core near the canopy centerline lessened the drag reduction brought on by the presence of the core.
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