Computational fluid dynamic studies of a solid and ribbon 12-gore parachute canopy in subsonic and supersonic flow-Reference-Cited by-同舟云学术

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Computational fluid dynamic studies of a solid and ribbon 12-gore parachute canopy in subsonic and supersonic flow

Published:1995-05-15 Issue: Volume: Page:
ISSN:
Container-title:13th Aerodynamic Decelerator Systems Technology Conference
language:
Short-container-title:

Author:

Nelsen James

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1995-1558

Reference10 articles.

1. Sundberg,W. D."ANew Solution Methodfor Steady-State CanopyStructural Luads",AIAA 86-2189. October 1986.

2. ABAQUSIExplicit User's Manual. Version 5.0,I-iibbitt, Karlsson &Sorenson Inc., Pawtucket, RI, 1991.

Cited by 7 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. Simulation of Drogue Parachute for the Multi-Purpose Crew Vehicle using Computational Fluid Dynamics;AIAA Aerodynamic Decelerator Systems (ADS) Conference;2013-03-23

2. A computational study of supersonic disk-gap-band parachutes using Large-Eddy Simulation coupled to a structural membrane;Journal of Fluids and Structures;2011-02

3. Aerodynamic Decelerators for Planetary Exploration: Past, Present, and Future;AIAA Guidance, Navigation, and Control Conference and Exhibit;2006-06-15

4. Structural Modeling of Parachute Dynamics;AIAA Journal;2000-01

5. Issues in parachute structural modeling - Damping and wrinkling;15th Aerodynamic Decelerator Systems Technology Conference;1999-06-08

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