Abstract
A numerical transient temperature analysis of a multiple carbon/carbon aircraft disc brake system is obtained using temperature dependent thermo-physical properties. Convective type boundary conditions are used. The maximum temperatures are found to occur around the middle disc and between the mid and outer radiuses of discs.
| Original language | English |
|---|---|
| State | Published - 1997 |
Bibliographical note
Publisher Copyright:© 1997 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
ASJC Scopus subject areas
- Mechanical Engineering
- Aerospace Engineering
- Condensed Matter Physics