Abstract
The Army currently lacks the ability to predict accurately the behavior of parachute fluid-structure interaction phenomena. The interactions between the parachute system and the surrounding flow field are dominant in most parachute operations and thus the ability to predict parachute fluid-structure interaction phenomena is of interest to the Army. This paper presents the current status of an ongoing research effort to couple the finite element formulations for the fluid dynamics and structural dynamics encountered in parachute problems. An application of the opening of an axisymmetric round parachute is presented. Future considerations for the coupled model and potential applications of interest to the Army are presented.
| Original language | English |
|---|---|
| Title of host publication | 14th Aerodynamic Decelerator Systems Technology Conference |
| Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
| Pages | 277-284 |
| Number of pages | 8 |
| DOIs | |
| Publication status | Published - 1997 |
| Externally published | Yes |
| Event | 14th Aerodynamic Decelerator Systems Technology Conference, 1997 - San Francisco, United States Duration: 1997 Jun 3 → 1997 Jun 5 |
Other
| Other | 14th Aerodynamic Decelerator Systems Technology Conference, 1997 |
|---|---|
| Country | United States |
| City | San Francisco |
| Period | 97/6/3 → 97/6/5 |
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ASJC Scopus subject areas
- Mechanical Engineering
- Aerospace Engineering
- Electrical and Electronic Engineering
Cite this
Parallel computation of parachute fluid-structure interactions. / Stein, Keith R.; Benney, Richard J.; Kalro, Vinay; Johnson, Andrew A.; Tezduyar, Tayfun E.
14th Aerodynamic Decelerator Systems Technology Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, 1997. p. 277-284 AIAA-97-1505.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
}
TY - GEN
T1 - Parallel computation of parachute fluid-structure interactions
AU - Stein, Keith R.
AU - Benney, Richard J.
AU - Kalro, Vinay
AU - Johnson, Andrew A.
AU - Tezduyar, Tayfun E.
PY - 1997
Y1 - 1997
N2 - The Army currently lacks the ability to predict accurately the behavior of parachute fluid-structure interaction phenomena. The interactions between the parachute system and the surrounding flow field are dominant in most parachute operations and thus the ability to predict parachute fluid-structure interaction phenomena is of interest to the Army. This paper presents the current status of an ongoing research effort to couple the finite element formulations for the fluid dynamics and structural dynamics encountered in parachute problems. An application of the opening of an axisymmetric round parachute is presented. Future considerations for the coupled model and potential applications of interest to the Army are presented.
AB - The Army currently lacks the ability to predict accurately the behavior of parachute fluid-structure interaction phenomena. The interactions between the parachute system and the surrounding flow field are dominant in most parachute operations and thus the ability to predict parachute fluid-structure interaction phenomena is of interest to the Army. This paper presents the current status of an ongoing research effort to couple the finite element formulations for the fluid dynamics and structural dynamics encountered in parachute problems. An application of the opening of an axisymmetric round parachute is presented. Future considerations for the coupled model and potential applications of interest to the Army are presented.
UR - http://www.scopus.com/inward/record.url?scp=84976484393&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84976484393&partnerID=8YFLogxK
U2 - 10.2514/6.1997-1505
DO - 10.2514/6.1997-1505
M3 - Conference contribution
SP - 277
EP - 284
BT - 14th Aerodynamic Decelerator Systems Technology Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
ER -