Transient temperature analysis of airplane carbon composite disk brakes


Sahin A. Z. , Al-Garni A. Z.

32nd Thermophysics Conference, 1997, Georgia, United States Of America, 23 - 25 June 1997 identifier

  • Publication Type: Conference Paper / Full Text
  • City: Georgia
  • Country: United States Of America

Abstract

© 1997 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.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.