Publikationsdatum:
2019-07-13
Beschreibung:
This paper explores use of computational fluid dynamics to study the eect of geometric porosity on static stability and drag for NASA's Multi-Purpose Crew Vehicle main parachute. Both of these aerodynamic characteristics are of interest to in parachute design, and computational methods promise designers the ability to perform detailed parametric studies and other design iterations with a level of control previously unobtainable using ground or flight testing. The approach presented here uses a canopy structural analysis code to define the inflated parachute shapes on which structured computational grids are generated. These grids are used by the computational fluid dynamics code OVERFLOW and are modeled as rigid, impermeable bodies for this analysis. Comparisons to Apollo drop test data is shown as preliminary validation of the technique. Results include several parametric sweeps through design variables in order to better understand the trade between static stability and drag. Finally, designs that maximize static stability with a minimal loss in drag are suggested for further study in subscale ground and flight testing.
Schlagwort(e):
Fluid Mechanics and Thermodynamics
Materialart:
JSC-CN-33012
,
AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar; Mar 30, 2015 - Apr 02, 2015; Daytona Beach, FL; United States
Format:
application/pdf
