Three-Component Velocity Field Measurements Near a Parachute During a Drop Test
Author:
Affiliation:
1. MetroLaser, Inc.
2. U.S. Army Natick Soldier Research, Development, and Engineering Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-1030
Reference12 articles.
1. Vortex shedding in the near wake of a parachute canopy
2. Computational methods for modeling parachute systems
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