Theoretical Analysis of Parachute Inflation Including Fluid Kinetics
Author:
Affiliation:
1. Sandia National Laboratories, Albuquerque, N. Mex.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.57392
Reference22 articles.
1. Aerodynamic decelerators - An engineering review
2. Recovery Systems Design Guide
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