Fluid structure interaction simulation of supersonic parachute inflation by an interface tracking method

Author:

YANG Xue,YU Li,LIU Min,PANG Haofei

Funder

National Nature Sciences Foundation of China

PAPD

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference39 articles.

1. Stevens GW. A model and calculation procedure for predicting parachute inflation. AIAA 4th aerodynamic deceleration systems conference; 1973 May 21–23; Palm Springs, USA. Reston: AIAA; 1973. p. 1–7.

2. Houmard JE. Stress analysis of the Viking parachute. AIAA 4th aerodynamic deceleration systems conference; 1973 May 21–23; Palm Springs, USA. Reston: AIAA; 1973. p. 1–12.

3. A simplified dynamic model of parachute inflation;Wolf;J Aircr,1973

4. Study of parachute inflation process using fluid–structure interaction method;Yu;Chin J Aeronaut,2014

5. Tutt BA, Taylor AP. The use of LS-DYNA to simulate the inflation of a parachute canopy. 18th AIAA aerodynamic decelerator systems technology conference and seminar. 2005 May 23-26. Virginia, USA. Reston: AIAA; 2005. p. 1–9.

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