Potential flowfield and added mass of the idealized hemispherical parachute.
Author:
Affiliation:
1. FluiDyne Engineering Corporation, Minneapolis, Minn.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.43803
Reference9 articles.
Cited by 15 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Added Mass of a Model Round Parachute Canopy during Inflation;AIAA Aerodynamic Decelerator Systems (ADS) Conference;2013-03-23
2. Unsteady Potential Flow Forces on an Inflating Parachute Canopy;17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar;2003-05-19
3. Three-dimensional vortex method for parachutes;International Journal for Numerical Methods in Fluids;1993-05-30
4. A prediction method for unsteady axisymmetric flow over parachutes;Aerospace Design Conference;1993-02-16
5. Drag computation by vortex methods;Journal of Aircraft;1992-09
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