SCOPUS 정보 검색 플랫폼

International SAMPE Symposium and Exhibition (Proceedings)

Volumn 46 I, Issue , 2001, Pages 1160-1173

Commercial application of composite doublers for DC-10 fuselage repairs

a SANDIA NATIONAL LABORATORIES (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADHESIVES; BONDING; CRACK PROPAGATION; FATIGUE OF MATERIALS; FIBER REINFORCED MATERIALS; NONDESTRUCTIVE EXAMINATION; STRESS INTENSITY FACTORS; STRUCTURAL LOADS;

COMPOSITE DOUBLERS;

COMPOSITE STRUCTURES;

EID: 0034824077 PISSN: 08910138 EISSN: None Source Type: Conference Proceeding
DOI: None Document Type: Conference Paper

Times cited : (2)

References (7)

1
- 0003536977
- Martinus Nijhoff Pub., The Netherlands
- (1988) Bonded Repair of Aircraft Structures
- Baker, A.A.¹ Jones, R.²

2
- 0141873734
- Growth characterization of fatigue cracks repaired with adhesively bonded boron/epoxy patches
- April
- (1997) Proc. Of Int'l Conf. Fracture , vol.ICF-9
- Baker, A.A.¹

3
- 0004023422
- Damage tolerance assessment of bonded composite doublers for commercial aircraft applications
- August
- (1998) Sandia National Laboratories/Dept. of Energy Report , vol.SAND98-1016
- Roach, D.P.¹

4
- 0003572820
- November
- (1997) FAA Report SNL96ER0189 under Atlanta Aircraft Certification Office Project SP1798AT-Q

5
- 0004023422
- Full scale structural and NDI validation tests on bonded composite doublers for commercial aircraft applications
- November
- (1998) Sandia National Laboratories/Dept. of Energy Report , vol.SAND98-1015
- Roach, D.P.¹ Walkington, P.²

6
- 0004023422
- Development and validation of nondestructive inspection techniques for composite doubler repairs on commercial aircraft applications
- May
- (1998) Sandia National Laboratories/Dept. of Energy Report , vol.SAND98-1014
- Roach, D.P.¹ Walkington, P.²

7
- 0003493191
- (1997) FAA Report SNL96ER0007 under Atlanta ACO Project SP1798AR-Q, FAA approval January 1997

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.