Parallel finite element computation of the dynamics of large ram air parachutes

S. K. Aliabadi; W. L. Garrard; V. Kalro; S. Mittal; T. E. Tezduyar; K. R. Stein

doi:10.2514/6.1995-1581

Parallel finite element computation of the dynamics of large ram air parachutes

S. K. Aliabadi, W. L. Garrard, V. Kalro, S. Mittal, T. E. Tezduyar, K. R. Stein

研究成果: Paper › 査読

14 被引用数 (Scopus)

抄録

Future airdrop systems require the development of very large gliding parachutes capable of delivering 21-ton payloads. This airdrop requirement presents new technology barriers which cannot be addressed by previous methods such as extensively costly airdrop testing and wind tunnel testing; hence the need to look towards high-performance computing as a viable alternative. In this paper we present a methodology to simulate the dynamics of ram-air parachutes using stabilized finite element Navier-Stokes solvers. Highly optimized coding techniques and algorithms provide us with the potential to solve systems with millions of coupled nonlinear equations. These computations are carried out on the massively parallel supercornputer CM-5.

本文言語	English
ページ	278-293
ページ数	16
DOI	https://doi.org/10.2514/6.1995-1581
出版ステータス	Published - 1995
外部発表	はい
イベント	13th AIAA Aerodynamic Decelerator Systems Technology Conference, 1995 - Clearwater Beach, United States 継続期間: 1995 5月 15 → 1995 5月 18

Other

Other	13th AIAA Aerodynamic Decelerator Systems Technology Conference, 1995
国/地域	United States
City	Clearwater Beach
Period	95/5/15 → 95/5/18

ASJC Scopus subject areas

航空宇宙工学
機械工学
電子工学および電気工学

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10.2514/6.1995-1581

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title = "Parallel finite element computation of the dynamics of large ram air parachutes",

abstract = "Future airdrop systems require the development of very large gliding parachutes capable of delivering 21-ton payloads. This airdrop requirement presents new technology barriers which cannot be addressed by previous methods such as extensively costly airdrop testing and wind tunnel testing; hence the need to look towards high-performance computing as a viable alternative. In this paper we present a methodology to simulate the dynamics of ram-air parachutes using stabilized finite element Navier-Stokes solvers. Highly optimized coding techniques and algorithms provide us with the potential to solve systems with millions of coupled nonlinear equations. These computations are carried out on the massively parallel supercornputer CM-5.",

author = "Aliabadi, {S. K.} and Garrard, {W. L.} and V. Kalro and S. Mittal and Tezduyar, {T. E.} and Stein, {K. R.}",

note = "Funding Information: This research was sponsored by ARO under grant, DAAH04-93-G-0514, by ARPA under NIST contract 60NANBZD1272, by NASA-JSC under grant NAG 9-449, and by the Army High Performance Computing Research Center under the auspices of the Department of the Army, Army Research Laboratory cooperative agreement number DAAH04-95-2-0003/contract number DAAH04-95-C-0008, the content of which does not necessarily reflect the position or the policy of the government, and no official endorsement should be inferred. Publisher Copyright: {\textcopyright} 1985 by the American Instituted Aeronautics and Astronautics, Inc. All rights reserved.; 13th AIAA Aerodynamic Decelerator Systems Technology Conference, 1995 ; Conference date: 15-05-1995 Through 18-05-1995",

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AU - Aliabadi, S. K.

AU - Garrard, W. L.

AU - Kalro, V.

AU - Mittal, S.

AU - Tezduyar, T. E.

AU - Stein, K. R.

N1 - Funding Information: This research was sponsored by ARO under grant, DAAH04-93-G-0514, by ARPA under NIST contract 60NANBZD1272, by NASA-JSC under grant NAG 9-449, and by the Army High Performance Computing Research Center under the auspices of the Department of the Army, Army Research Laboratory cooperative agreement number DAAH04-95-2-0003/contract number DAAH04-95-C-0008, the content of which does not necessarily reflect the position or the policy of the government, and no official endorsement should be inferred. Publisher Copyright: © 1985 by the American Instituted Aeronautics and Astronautics, Inc. All rights reserved.

PY - 1995

Y1 - 1995

N2 - Future airdrop systems require the development of very large gliding parachutes capable of delivering 21-ton payloads. This airdrop requirement presents new technology barriers which cannot be addressed by previous methods such as extensively costly airdrop testing and wind tunnel testing; hence the need to look towards high-performance computing as a viable alternative. In this paper we present a methodology to simulate the dynamics of ram-air parachutes using stabilized finite element Navier-Stokes solvers. Highly optimized coding techniques and algorithms provide us with the potential to solve systems with millions of coupled nonlinear equations. These computations are carried out on the massively parallel supercornputer CM-5.

AB - Future airdrop systems require the development of very large gliding parachutes capable of delivering 21-ton payloads. This airdrop requirement presents new technology barriers which cannot be addressed by previous methods such as extensively costly airdrop testing and wind tunnel testing; hence the need to look towards high-performance computing as a viable alternative. In this paper we present a methodology to simulate the dynamics of ram-air parachutes using stabilized finite element Navier-Stokes solvers. Highly optimized coding techniques and algorithms provide us with the potential to solve systems with millions of coupled nonlinear equations. These computations are carried out on the massively parallel supercornputer CM-5.

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T2 - 13th AIAA Aerodynamic Decelerator Systems Technology Conference, 1995

Y2 - 15 May 1995 through 18 May 1995

ER -

Parallel finite element computation of the dynamics of large ram air parachutes

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