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Titolo:
DESIGN OF HYBRID COMPOSITES WITH ZERO COEFFICIENT OF THERMAL-EXPANSION
Autore:
ZHANG ZG; ZHONG WH; SONG HC;
Indirizzi:
BEIJING UNIV AERONAUT & ASTRONAUT,DEPT MAT SCI & ENGN BEIJING 100083 PEOPLES R CHINA BEIJING UNIV AERONAUT & ASTRONAUT,DEPT MAT SCI & ENGN BEIJING 100083 PEOPLES R CHINA
Titolo Testata:
JOURNAL OF MATERIALS SCIENCE & TECHNOLOGY
fascicolo: 4, volume: 12, anno: 1996,
pagine: 241 - 248
SICI:
1005-0302(1996)12:4<241:DOHCWZ>2.0.ZU;2-N
Fonte:
ISI
Lingua:
ENG
Tipo documento:
Article
Natura:
Periodico
Settore Disciplinare:
Science Citation Index Expanded
Science Citation Index Expanded
Citazioni:
3
Recensione:
Indirizzi per estratti:
Citazione:
Z.G. Zhang et al., "DESIGN OF HYBRID COMPOSITES WITH ZERO COEFFICIENT OF THERMAL-EXPANSION", JOURNAL OF MATERIALS SCIENCE & TECHNOLOGY, 12(4), 1996, pp. 241-248

Abstract

Structures used in aerospace are influenced by temperature. So coefficient-of thermal expansion (CTE) is not only an important parameter ofmaterials, but also a significant parameter of structural design of spacecrafts with high dimensional stability. In this paper, based on the analysis of the data from tests, theoretical formulae for predictingCTE and mechanical properties of hybrid composites are presented, andthe calculation program is compiled. All the equations are verified by experiments. Optimization is conducted by computer. The results and methods presented in this paper can be used both in optimal design of hybrid composites with zero CTE and in design of hybrid composites with any certain CTE value.

ASDD Area Sistemi Dipartimentali e Documentali, Università di Bologna, Catalogo delle riviste ed altri periodici
Documento generato il 08/07/20 alle ore 07:58:47