Tire Runway Interface Friction Prediction Subsystem.
Abstract
An analytical tire model was developed that correlates with existing tire test data to within + or - 5%. The model consists of a prediction equation expressing the relationships between seven dimensionless groups (pi terms) needed to define the aircraft tire-runway interface friction. A tire test program was recommended to validate the said model. A specification criteria has been established for the interface Friction Prediction Subsystem and various ground vehicles in use to date were evaluated. None of the vehicles meets the specification criteria.
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 01, 1977
- Accession Number
- ADA039968
Entities
People
- H. H. Straub
- M. K. Wahi
Organizations
- Boeing Commercial Airplanes