Highly Dynamic Sled System for Comprehensive Seat Development

ATZ worldwide ◽  
2015 ◽  
Vol 117 (7-8) ◽  
pp. 4-9
Author(s):  
Valentin Zimmermann ◽  
Rainer Freimark ◽  
Martin Floßmann
Keyword(s):  
Author(s):  
J. P. Coakley ◽  
H. A. Savile ◽  
M. Pedrosa ◽  
M. Larocque
Keyword(s):  

2000 ◽  
Vol 39 (Part 1, No. 2B) ◽  
pp. 843-845 ◽  
Author(s):  
Jinsong Han ◽  
Kai Meng Hock ◽  
Wenhua Li ◽  
Tow Chong Chong ◽  
Kenji Shintani ◽  
...  

Author(s):  
Raymond Rayaraj ◽  
Jinsong Han ◽  
Wenhua Li ◽  
Kai Meng Hock ◽  
Kenji Shintani ◽  
...  

1978 ◽  
Vol 1 (16) ◽  
pp. 106 ◽  
Author(s):  
J.P. Coakley ◽  
H.A. Savile ◽  
M. Pedrosa ◽  
M. Larocque

There are many factors which suggest that littoral zone processes in the Great Lakes differ substantially from those of the marine coasts described in the existing coastal research literature. Among these factors are the lack of an appreciable tidal cycle; the predominance of relatively short, steep, waves; the virtual absence of swell waves; and the presence of shore fast ice in winter. As a result, many of the empirical relationships derived for marine coasts might be of questionable applicability to Great Lakes coasts. The present study, which represents only one phase of a long-term project designed to develop more specific littoral transport relationships, is aimed at obtaining accurate, direct estimates of the actual littoral transport at an experimental site located at the western end of Lake Ontario. This paper will describe a mechanical system designed to collect a series of time-averaged samples of suspended sediment for concentration determinations as well as flow velocity and water depth at locations across the surf zone. Some preliminary results of the field program using the system will also be presented and discussed.


Author(s):  
Xuewen Zhou ◽  
Jian Xu ◽  
Shuiyan Lv

Ground-based methods for accurately representing high-altitude, high-speed flight conditions have been an important research topic in the aerospace field. Based on an analysis of the requirements for high-altitude supersonic flight tests, a ground-based test bed was designed combining Laval nozzle, which is often found in wind tunnels, with a rocket sled system. Sled tests were used to verify the performance of the test bed. The test results indicated that the test bed produced a uniform-flow field with a static pressure and density equivalent to atmospheric conditions at an altitude of 13–15[Formula: see text]km and at a flow velocity of approximately M 2.4. This test method has the advantages of accuracy, fewer experimental limitations, and reusability.


Author(s):  
C R Bass ◽  
J R Crandall ◽  
E Dekel ◽  
A Jordan ◽  
W D Pilkey

A sled system capable of producing structural intrusion in the footwell region of an automobile has been developed. The system couples the hydraulic decelerator of the sled to actuator pistons attached to the toepan and floorpan structure of the buck. Characterization of the footwell intrusion event is based on developing a toepan pulse analogous to the acceleration pulse used to characterize sled and vehicle decelerations. Sled tests with the system indicate that it is capable of accurately and repeatably simulating toepan/floorpan intrusion into the occupant footwell. Test results, including a comparison of lower extremity response between intrusion sled tests and no intrusion sled tests, indicate that this system is capable of repeatable, controlled structural intrusion during a sled test impact. Test results also suggest that lower extremity forcing during footwell intrusion is significantly larger than such forcing with no intrusion, and that response and risk of injury for occupants in frontal or frontal-offset crashes are more severe.


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