Simulation of parachute dynamics during control line input operations

K. Stein; T. Tezduyar; S. Sathe; M. Senga; C. Ozcan; T. Soltys; V. Kumar; R. Benney; R. Charles

Simulation of parachute dynamics during control line input operations

K. Stein, T. Tezduyar, S. Sathe, M. Senga, C. Ozcan, T. Soltys, V. Kumar, R. Benney, R. Charles

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Abstract

An approach for the numerical simulation of parachute fluid-structure interactions is highlighted. Numerical examples are presented demonstrating the fluid-structure interaction behavior for a steerable round parachute and for a parachute soft-landing retraction system. For the fluid dynamics simulations, we use the Deforming-Spatial-Domain/Stabilized Space-Time (DSD/SST) formulation which was developed for flow problems with moving boundaries and interfaces,¹ along with an automatic mesh update method and occasional remeshing of the fluid mesh. The structural dynamics simulations utilize a finite element formulation based on the principle of virtual work for a cable-membrane tension structure.².

Original language	English
Title of host publication	17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar
Publication status	Published - 2003
Externally published	Yes
Event	17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar 2003 - Monterey, CA, United States Duration: 2003 May 19 → 2003 May 22

Publication series

Name	17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar

Other

Other	17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar 2003
Country/Territory	United States
City	Monterey, CA
Period	03/5/19 → 03/5/22

ASJC Scopus subject areas

Aerospace Engineering
Electrical and Electronic Engineering
Mechanical Engineering

Cite this

Stein, K, Tezduyar, T, Sathe, S, Senga, M, Ozcan, C, Soltys, T, Kumar, V, Benney, R & Charles, R 2003, Simulation of parachute dynamics during control line input operations. in 17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar. 17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, 17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar 2003, Monterey, CA, United States, 03/5/19.

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title = "Simulation of parachute dynamics during control line input operations",

abstract = "An approach for the numerical simulation of parachute fluid-structure interactions is highlighted. Numerical examples are presented demonstrating the fluid-structure interaction behavior for a steerable round parachute and for a parachute soft-landing retraction system. For the fluid dynamics simulations, we use the Deforming-Spatial-Domain/Stabilized Space-Time (DSD/SST) formulation which was developed for flow problems with moving boundaries and interfaces,1 along with an automatic mesh update method and occasional remeshing of the fluid mesh. The structural dynamics simulations utilize a finite element formulation based on the principle of virtual work for a cable-membrane tension structure.2.",

author = "K. Stein and T. Tezduyar and S. Sathe and M. Senga and C. Ozcan and T. Soltys and V. Kumar and R. Benney and R. Charles",

year = "2003",

language = "English",

isbn = "9781624100871",

series = "17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar",

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note = "17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar 2003 ; Conference date: 19-05-2003 Through 22-05-2003",

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T1 - Simulation of parachute dynamics during control line input operations

AU - Stein, K.

AU - Tezduyar, T.

AU - Sathe, S.

AU - Senga, M.

AU - Ozcan, C.

AU - Soltys, T.

AU - Kumar, V.

AU - Benney, R.

AU - Charles, R.

PY - 2003

Y1 - 2003

N2 - An approach for the numerical simulation of parachute fluid-structure interactions is highlighted. Numerical examples are presented demonstrating the fluid-structure interaction behavior for a steerable round parachute and for a parachute soft-landing retraction system. For the fluid dynamics simulations, we use the Deforming-Spatial-Domain/Stabilized Space-Time (DSD/SST) formulation which was developed for flow problems with moving boundaries and interfaces,1 along with an automatic mesh update method and occasional remeshing of the fluid mesh. The structural dynamics simulations utilize a finite element formulation based on the principle of virtual work for a cable-membrane tension structure.2.

AB - An approach for the numerical simulation of parachute fluid-structure interactions is highlighted. Numerical examples are presented demonstrating the fluid-structure interaction behavior for a steerable round parachute and for a parachute soft-landing retraction system. For the fluid dynamics simulations, we use the Deforming-Spatial-Domain/Stabilized Space-Time (DSD/SST) formulation which was developed for flow problems with moving boundaries and interfaces,1 along with an automatic mesh update method and occasional remeshing of the fluid mesh. The structural dynamics simulations utilize a finite element formulation based on the principle of virtual work for a cable-membrane tension structure.2.

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M3 - Conference contribution

AN - SCOPUS:84894808229

SN - 9781624100871

T3 - 17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar

BT - 17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar

T2 - 17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar 2003

Y2 - 19 May 2003 through 22 May 2003

ER -

Simulation of parachute dynamics during control line input operations

Abstract

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ASJC Scopus subject areas

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