Dynamics Simulation of Sounding Rocket Water Landing Recovery with Fluid-Structure Interaction Method

Wei Zhou; Xuan Yang; Hua Yang

doi:10.4028/www.scientific.net/AMM.470.220

Paper Titles

Finite Element Simulation Analysis of Multi-Stands Three-Roller Cold Rolling Process for Double Metal Composite Seamless Steel Tube
p.197

Numerical Simulation Analysis on Stability of Coal Pillar of Empty Mine Goaf in North of Shanxi Province
p.205

Test-Bench Design for Fiber Paying-Off Simulating
p.211

The Finite Element Analysis of Batching Machine Spindle Based on ANSYS
p.216

Dynamics Simulation of Sounding Rocket Water Landing Recovery with Fluid-Structure Interaction Method
p.220

Research on the Semi-Physical Simulation Technology of High Pressure Common Rail Electronic Control System for Low-Speed Marine Diesel Engine
p.226

Nonlinear Finite Element Analysis for Galloping of Iced Quad-Bundled Conductor
p.232

The Establishment of Distribution Model of Inner Surface Pressure of Elbow Pipe Based on FLUENT
p.236

Time Series Modeling of Earthquake Ground Motions Using ARMA-GARCH Models
p.240

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 470Dynamics Simulation of Sounding Rocket Water...

Dynamics Simulation of Sounding Rocket Water Landing Recovery with Fluid-Structure Interaction Method

Abstract:

This paper presents the water landing dynamics simulation of a sounding rocket, obtaining dynamics characteristics of the interaction between the rocket payload module, the floatation airbag and the water. Using an explicit nonlinear dynamic finite element code, the model contains Lagrangian shell elements for rocket payload, membrane elements for the airbag and Eulerian elements for the water. The Fluid-Structure Interaction (FSI) technology is employed in the computation by transferring forces on nodes of coupling surfaces. In the paper, two landing attitudes are analyzed and compared. After analyzing dynamic response of airbag under different operating conditions, the minimum size is concluded. This dynamics simulation builds the foundation for the Engineering Model of the recovery system.

You might also be interested in these eBooks

Mechanical Engineering, Materials Science and Civil Engineering II

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volume 470)

Pages:

220-225

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.470.220

Citation:

Cite this paper

Online since:

December 2013

Authors:

Wei Zhou*, Xuan Yang, Hua Yang

Keywords:

Floatation Airbag, Recovery, Sounding Rocket

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

* - Corresponding Author

References

[1] JIANG Xiujie, et al. Development Status and Trend of Sounding Rocket [J]. Science & Technology Review, 2009, 27(23): 101~110.

Google Scholar

[2] Dytran 2010 User's Guide, MSC Software Corporation.

Google Scholar

[3] HE Huan, et al. Modeling and Simulation of Landing Procedure of Multi-cavity Airbag Cushion Recovery System [J]. Journal of Nanjing University of Aeronautics & Astronautics, 2013, 45(1): 08~12.

Google Scholar

[4] CUI Yihua, Research on airbag materials and the design [J]. Journal of Textile Research, 2004, 25(6): 133~134.

Google Scholar