An Investigation of the Apparent Mass of Parachutes Under Post Inflation Dynamic Loading Through the use of Fluid Structure Interaction Simulations-Reference-Cited by-同舟云学术

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An Investigation of the Apparent Mass of Parachutes Under Post Inflation Dynamic Loading Through the use of Fluid Structure Interaction Simulations

Published:2003-05-19 Issue: Volume: Page:
ISSN:
Container-title:17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar
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Author:

Taylor T.¹

Affiliation:

1. Irvin Aerospace Inc

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-2104

Cited by 9 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. Development and Validation of a Nonlinear Fabric Model for Subsonic Parachute Aerodynamics;Journal of Spacecraft and Rockets;2023-11

2. Numerical Study of Aerodynamic Characteristics of No-Swinging and Free-to-Swing Cross Parachute;AIAA Journal;2023-11

3. Experimental investigation of the flow structures in the wake of a cross parachute canopy;European Journal of Mechanics - B/Fluids;2016-11

4. References;Precision Aerial Delivery Systems: Modeling, Dynamics, and Control;2015-01-01

5. Improvements in Fluid Structure Interaction Simulations of Parachutes Using LS-Dyna®;21st AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar;2011-05-23

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