RABEEH, B., MOUSSA, M., MOHAMED, M., EL- HADDAD, M. (1999). ALUMINUM METAL MATRIX COMPOSITES IN AEROSPACE APPLICATIONS. test, 8(ASAT Conference, 4-6 May 1999), 1-12. doi: 10.21608/asat.1999.25083
B. M. RABEEH; M. M. MOUSSA; M. Y. MOHAMED; M. A. EL- HADDAD. "ALUMINUM METAL MATRIX COMPOSITES IN AEROSPACE APPLICATIONS". test, 8, ASAT Conference, 4-6 May 1999, 1999, 1-12. doi: 10.21608/asat.1999.25083
RABEEH, B., MOUSSA, M., MOHAMED, M., EL- HADDAD, M. (1999). 'ALUMINUM METAL MATRIX COMPOSITES IN AEROSPACE APPLICATIONS', test, 8(ASAT Conference, 4-6 May 1999), pp. 1-12. doi: 10.21608/asat.1999.25083
RABEEH, B., MOUSSA, M., MOHAMED, M., EL- HADDAD, M. ALUMINUM METAL MATRIX COMPOSITES IN AEROSPACE APPLICATIONS. test, 1999; 8(ASAT Conference, 4-6 May 1999): 1-12. doi: 10.21608/asat.1999.25083

ALUMINUM METAL MATRIX COMPOSITES IN AEROSPACE APPLICATIONS

International Conference on Aerospace Sciences and Aviation Technology
Article 34, Volume 8, ASAT Conference, 4-6 May 1999, May 1999, Pages 1-12    PDF (2.49 M)
Document Type: Original Article
DOI: 10.21608/asat.1999.25083
Authors
B. M. RABEEH1; M. M. MOUSSA2; M. Y. MOHAMED2; M. A. EL- HADDAD2
1Department of Materials Science and Engineering, MTC, Cairo.
2Department of Automotive Engineering, MTC, Cairo.
Abstract
The aerospace industry's constant desire to enhance the performance of commercial and military aircrafts is continually driving the development of improved high - performance structural materials. In recent years, Metal-matrix composites (MMC) have emerged as a promising class of materials. Especially, Aluminum composites with their unique thermal properties have enormous space and avionics prospects. Al-matrix composites have the potential of achieving significant weight and cost savings on aircraft structures. In this paper, the fabrication and properties of the Al-matrix composites and their scopes in aerospace industries will be reviewed in details. Besides, recently Hot lsostatic Pressed (HIPed) Al-matrix composites reinforced with steel fibers and its evaluating parameters will be discussed with microstructure changes and mechanical behavior.
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