Transient temperature analysis of airplane carbon composite disk brakes

Ahmet Z. Sahin; Ahmed Z. Al-Garni

Transient temperature analysis of airplane carbon composite disk brakes

Ahmet Z. Sahin
, Ahmed Z. Al-Garni

King Fahd University of Petroleum and Minerals

Araştırma sonucu: Konferansa katkı › Yazı › bilirkişi

Özet

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.

Orijinal dil	İngilizce
Yayın durumu	Yayınlandı - 1997
Harici olarak yayınlandı	Evet
Etkinlik	32nd Thermophysics Conference, 1997 - Atlanta, United States Süre: 23 Haz 1997 → 25 Haz 1997

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???event.eventtypes.event.conference???	32nd Thermophysics Conference, 1997
Ülke/Bölge	United States
Şehir	Atlanta
Periyot	23/06/97 → 25/06/97

Bibliyografik not

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

Diğer Dosyalar ve Linkler

Link to publication in Scopus

Alıntı Yap

@conference{dead9d2435564d789975dbf90a134c94,

title = "Transient temperature analysis of airplane carbon composite disk brakes",

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.",

author = "Sahin, \{Ahmet Z.\} and Al-Garni, \{Ahmed Z.\}",

note = "Publisher Copyright: {\textcopyright} 1997 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.; 32nd Thermophysics Conference, 1997 ; Conference date: 23-06-1997 Through 25-06-1997",

year = "1997",

language = "English",

}

TY - CONF

T1 - Transient temperature analysis of airplane carbon composite disk brakes

AU - Sahin, Ahmet Z.

AU - Al-Garni, Ahmed Z.

PY - 1997

Y1 - 1997

N2 - 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.

AB - 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.

UR - https://www.scopus.com/pages/publications/84964053059

M3 - Paper

AN - SCOPUS:84964053059

T2 - 32nd Thermophysics Conference, 1997

Y2 - 23 June 1997 through 25 June 1997

ER -

Transient temperature analysis of airplane carbon composite disk brakes

Özet

???event.eventtypes.event.conference???

Bibliyografik not

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