@inproceedings{fc234047a08345898626b1e98483fad4,
title = "Simulation and analysis of ballute decelerating system",
abstract = "A ballute is an inflatable, aerodynamic drag device and can provide efficient drag in a wide speed regime. In this paper, two ballute shapes have been proposed and studied in order to obtain relatively optimum configuration with maximum drag. This study simulates the flow fields of the optimum ballute configuration to investigate its aerodynamic performance at Mach numbers from 0.3 to 2.0. The burble fence and the air inlets are important components of a ballute whose effects on the decelerating performance were considered as well.",
author = "Bing Chen and Hong Xu and Zhixiu Xu and Weiliang He",
note = "Publisher Copyright: {\textcopyright} 2015, AIAA American Institute of Aeronautics and Astronautics. All rights reserved.; 23rd AIAA Aerodynamic Decelerator Systems Technology Conference, 2015 ; Conference date: 30-03-2015 Through 02-04-2015",
year = "2015",
doi = "10.2514/6.2015-2160",
language = "英语",
series = "Aerodynamic Decelerator Systems Technology Conferences",
publisher = "AIAA American Institute of Aeronautics and Astronautics",
booktitle = "Aerodynamic Decelerator Systems Technology Conferences",
}