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  • https://doi.org/10.2514/6.2013-1384Copy DOI Icon

Fluid Structure Interaction Parachute Benchmark Models in LS-DYNA

  • Mar 23, 2013
  • Benjamin A Tutt
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Abstract

This paper describes the development and results of numerical models describing system level parachute performance. The numerical models were developed to replicate a series of parachute drop tests conducted in the early 1950s. Wright Air Development Division Report AFTR 5867 documents 700 parachute drop tests, using twenty seven different parachutes, at the Goodyear Aircraft Corporation airship dock in Akron, Ohio between 1952 and 1954. The data from these tests were compiled into charts and referenced in the Parachute Recovery Systems Design Manual (T.W. Knacke). The numerical models were developed using Fluid Structure Interaction (FSI) techniques in the commercially available transient dynamic finite element code LS-DYNA. This paper describes the development of an 11.9 ft Nominal Diameter (D0) 10% extended skirt parachute model. Parachute drag, maximum oscillation angle, and frequency of oscillation are calculated for the parachute for ranges of rate of descent and suspension line length ratio, and compared with test data from AFTR 5867. This paper proposes a benchmarking parachute test series for current and future FSI numerical models.

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