NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
NASA evaluation of Type 2 chemical depositionsRecent findings from NASA Langley tests to define effects of aircraft Type 2 chemical deicer depositions on aircraft tire friction performance are summarized. The Aircraft Landing Dynamics Facility (ALDF) is described together with the scope of the tire cornering and braking friction tests conducted up to 160 knots ground speed. Some lower speed 32 - 96 km/hr (20 - 60 mph) test run data obtained using an Instrumented Tire Test Vehicle (ITTV) to determine effects of tire bearing pressure and transverse grooving on cornering friction performance are also discussed. Recommendations are made concerning which parameters should be evaluated in future testing.
Document ID
19950058487
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Yager, Thomas J. (NASA Langley Research Center Hampton, VA, United States)
Stubbs, Sandy M. (NASA Langley Research Center Hampton, VA, United States)
Howell, W. Edward (NASA Langley Research Center Hampton, VA, United States)
Webb, Granville L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
ISSN: 0148-7191
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
SAE PAPER 932582
Meeting Information
Meeting: SAE, Aerotech ''93
Location: Costa Mesa, CA
Country: United States
Start Date: September 27, 1993
End Date: September 30, 1993
Accession Number
95A90086
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available