SCOPUS 정보 검색 플랫폼

Journal of Composite Materials

Volumn 31, Issue 15, 1997, Pages 1534-1554

Microstructural differences between woven mat and acrylic binder TMC and their relationship to fatigue damage modes

(3) Harmon, D a Jerina, K L b,c Sastry, S M L b

a BOEING COMPANY (United States)

b WASHINGTON UNIVERSITY (United States)

c Mat Science and Engineering Program (United States)

Author keywords

Crack growth; Damage; Fatigue life; Scanning electron microscopy; Titanium matrix composites

Indexed keywords

AUGER ELECTRON SPECTROSCOPY; BINDERS; CONSOLIDATION; CRACK PROPAGATION; FATIGUE OF MATERIALS; METALLOGRAPHIC MICROSTRUCTURE; OPTICAL MICROSCOPY; PRESSURE EFFECTS; SCANNING ELECTRON MICROSCOPY; THERMAL EFFECTS; TITANIUM; X RAY ANALYSIS;

ENERGY DISPERSIVE X RAY ANALYSIS (EDX); FATIGUE DAMAGE MODES;

METALLIC MATRIX COMPOSITES;

EID: 0030658482 PISSN: 00219983 EISSN: None Source Type: Journal
DOI: 10.1177/002199839703101504 Document Type: Article

Times cited : (2)

References (7)

1
- 5844371559
- Lisagor, B. W. 1991. Advanced Metallics for High Temperature Airframe Structures.
- (1991) Advanced Metallics for High Temperature Airframe Structures
- Lisagor, B.W.¹

2
- 5844379597
- Hypersonic Materials
- Colucci, F. 1991. "Hypersonic Materials," Aerospace Composites & Materials, 3(6):4-8.
- (1991) Aerospace Composites & Materials , vol.3 , Issue.6 , pp. 4-8
- Colucci, F.¹

3
- 5844368175
- AFWAL-TR-87-3060, October
- Harmon, D. M., C. R. Saff and C. T. Sun. 1987. "Durability of Continuous Fiber Reinforced Metal Matrix Composites-Final Report," AFWAL-TR-87-3060, October.
- (1987) Durability of Continuous Fiber Reinforced Metal Matrix Composites-Final Report
- Harmon, D.M.¹ Saff, C.R.² Sun, C.T.³

4
- 5844400908
- WL-TR-94-3015, Contract No. F33615-87-C-3219, McDonnell Aircraft Company
- Harmon, D. M. and M. A. Finefield. 1994. "Thermomechanical Load History Effects in Metal Matrix Composites-Final Report," WL-TR-94-3015, Contract No. F33615-87-C-3219, McDonnell Aircraft Company.
- (1994) Thermomechanical Load History Effects in Metal Matrix Composites-Final Report
- Harmon, D.M.¹ Finefield, M.A.²

5
- 0026896370
- Crack Initiation around Holes in a Unidirectional MMC under Faligue Loading
- Newaz, G. M. and B. S. Majumdar, 1992. "Crack Initiation around Holes in a Unidirectional MMC under Faligue Loading." Engineering Fracture Mechanics, 42(4):699.
- (1992) Engineering Fracture Mechanics , vol.42 , Issue.4 , pp. 699
- Newaz, G.M.¹ Majumdar, B.S.²

6
- 84914776765
- Damage Initiation and Growth in Fiber Reinforced Metal Matrix Composites
- W. S. Johnson, ed., ASTM STP 1032. American Society for Testing and Materials. Philadelphia
- Harmon, D. M. and C. R. Saff. 1989. "Damage Initiation and Growth in Fiber Reinforced Metal Matrix Composites." Metal Matrix Composites: Testing, Analysis, and Failure Modes, W. S. Johnson, ed., ASTM STP 1032. American Society for Testing and Materials. Philadelphia, pp. 237-250.
- (1989) Metal Matrix Composites: Testing, Analysis, and Failure Modes , pp. 237-250
- Harmon, D.M.¹ Saff, C.R.²

7
- 0041343033
- TP 2970. NASA Lewis Research Center
- Lerch. B. A., T. P. Gabb and R. A. MacKay. 1990. "Heat Treatment Study of the SiC/Ti-15-3 Composite System," TP 2970. NASA Lewis Research Center.
- (1990) Heat Treatment Study of the SiC/Ti-15-3 Composite System
- Lerch, B.A.¹ Gabb, T.P.² MacKay, R.A.³

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.