Volume 47, Issue 6-7 pp. 619-631
Research Article

Fluid–structure interaction modelling of parachute soft-landing dynamics

Keith Stein

Corresponding Author

Keith Stein

Department of Physics, Bethel University, St. Paul, MN, 55112, U.S.A.

Department of Physics, Bethel University, St. Paul, MN, 55112, U.S.A.===Search for more papers by this author
Tayfun E. Tezduyar

Tayfun E. Tezduyar

Mechanical Engineering, Rice University, MS 321, 6100 Main Street, Houston, TX 77005, U.S.A.

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Sunil Sathe

Sunil Sathe

Mechanical Engineering, Rice University, MS 321, 6100 Main Street, Houston, TX 77005, U.S.A.

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Richard Benney

Richard Benney

U.S. Army Natick Soldier Center, Kansas Street, Natick, MA, 10760, U.S.A.

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Richard Charles

Richard Charles

U.S. Army Natick Soldier Center, Kansas Street, Natick, MA, 10760, U.S.A.

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First published: 17 December 2004
Citations: 13

Abstract

Soft landing of a payload with the aid of a retraction device is an important aspect in cargo parachute operations. Accurate simulation of this class of parachute operations with a computer model that takes into account the fluid–structure interactions involved would complement drop tests and support the design of cargo parachute systems. We describe the computational methods developed for this purpose, demonstrate how the computational model works in investigation of different soft-landing conditions, and show a good correlation between the data from our simulations and drop tests. Copyright © 2004 John Wiley & Sons, Ltd.

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