3-D parachute descent analysis using coupled CFD and structural codes-Reference-Cited by-同舟云学术

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3-D parachute descent analysis using coupled CFD and structural codes

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

Author:

Sahu Jubaraj,Cooper Gene,Benney Richard

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1995-1580

Reference15 articles.

1. Maydew, R.C., Peterson, C.W., and Orlik-Ruckemann, K.J. "Design and Testing of High-PerformanceParachutes,"AGARDographNo.319, November 1991.

2. Recovery Systems Design Guide

3. Performance of and Design Criteria for Deployable Aerodynamic Decelerators, USAF ASD-TR-61-597,December 1963.

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1. Computational Investigation on the Wake Flow of a Hemispherical Parachute Canopy;24th AIAA Aerodynamic Decelerator Systems Technology Conference;2017-06-02

2. Numerical simulation of parachute Fluid-Structure Interaction in terminal descent;Science China Technological Sciences;2012-09-07

3. Numerical simulation of the flow field around parachute during terminal descent;Aircraft Engineering and Aerospace Technology;2007-05-22

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

5. Experimental analysis of the pressure distribution on a 35-foot personnel parachute;16th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar;2001-05-21

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