Kramer, R and Cirak, F and Cirak, F and Pantano, C (2010) Fluid-structure interaction simulation of an inflatable aerodynamic tension-cone decelerator. 40th AIAA Fluid Dynamics Conference.Full text not available from this repository.
Inflatable aerodynamic decelerators have potential advantages for planetary re-entry in robotic and human exploration missions. In this paper, we focus on an inflatable tension cone design that has potential advantages over other geometries. A computational fluid-structure interaction model of a tension cone is employed to investigate the behavior of the inflatable aeroshell at supersonic speeds for conditions matching recent experimental results. A parametric study is carried out to investigate the deflections of the tension cone as a function of inflation pressure of the torus at a Mach of 2.5. Comparison of the behavior of the structure, amplitude of deformations, and determined loads are reported. © 2010 by the American Institute of Aeronautics and Astronautics, Inc.
|Divisions:||Div D > Structures|
|Depositing User:||Cron job|
|Date Deposited:||16 Jul 2015 14:12|
|Last Modified:||30 Aug 2015 04:31|