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contributor authorT. Snyder
contributor authorJ. Sitter
contributor authorJ. N. Chung
date accessioned2017-05-08T23:52:52Z
date available2017-05-08T23:52:52Z
date copyrightDecember, 1997
date issued1997
identifier issn0022-0434
identifier otherJDSMAA-26241#631_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/118359
description abstractThe design and performance evaluation of an airbag system capable of decelerating masses in the range of hundreds to thousands of kilograms with impact velocities in the range of tens to hundreds of kilometers per hour is presented. First, a simplified incompressible flow analysis of the airbag is utilized to derive the orifice venting area corresponding to the ideal deceleration for a given impact velocity and package mass. Second, testing with a small-scale model found three distinct control intervals during the deceleration. Finally, a full-scale airbag system was constructed and data is presented on the deceleration, deceleration force, deceleration velocity, airbag stopping power, and overall performance. The deceleration was experimentally optimized for a single impact velocity and package mass and an approximate correction factor was developed to predict the actual air venting required for each of the three control intervals in order to achieve the optimum deceleration for any impact velocity and package mass.
publisherThe American Society of Mechanical Engineers (ASME)
titleDesign and Testing of an Airbag System for High-Mass, High-Velocity Deceleration
typeJournal Paper
journal volume119
journal issue4
journal titleJournal of Dynamic Systems, Measurement, and Control
identifier doi10.1115/1.2802371
journal fristpage631
journal lastpage637
identifier eissn1528-9028
treeJournal of Dynamic Systems, Measurement, and Control:;1997:;volume( 119 ):;issue: 004
contenttypeFulltext


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