Recent findings from NASA Langley tests to define effects of aircraft Type II 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.
NASA Evaluation of Type II Chemical Depositions
Sae Technical Papers
Aerospace Technology Conference and Exposition ; 1993
1993-09-01
Aufsatz (Konferenz)
Englisch
NASA evaluation of Type 2 chemical depositions
NTRS | 1993
|NTRS | 2008
|British Library Online Contents | 2002
|NTIS | 2008
|NASA Chemical Propulsion In-Space
NTIS | 2018
|