NDLI: Review of antiskid and brake dynamics research

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Review of antiskid and brake dynamics research

Content Provider	NASA Technical Reports Server (NTRS)
Author	Tanner, J. A. Stubbs, S. M.
Copyright Year	1981
Description	The behavior of various antiskid systems was investigated under controlled conditions. Results from utilizing a single main wheel of a DC-9 aircraft suggest that the systems investigated perform well under most circumstances but there may be room for improvement. For example, it was demonstrated that pressure bias modulation can adversely affect the response of antiskid systems to rapid changes in the runway friction level. Results also indicate that antiskid systems designed to operate at a slip ratio of approximately 0.1 can provide a maximum braking effort without undue loss in the cornering capability of the tire. Time histories of braking friction coefficient were shown to provide a means of determining antiskid system performance and for systems that employed pressure bias modulation it was shown that performance could also be estimated from time histories of brake pressure and torque.
File Size	3277616
Page Count	14
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19810010540
Archival Resource Key	ark:/13960/t9t19tm8b
Language	English
Publisher Date	1981-03-01
Access Restriction	Open
Subject Keyword	Air Transportation And Safety Dynamic Response Coefficient of Friction Safety Devices Runways Aircraft Performance Antiskid Devices Aircraft Brakes Mathematical Models Wheel Brakes Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Article

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