SCOPUS 정보 검색 플랫폼

Volumn 10, Issue 3, 2001, Pages 490-496

Experimental analysis of buckling in aircraft skin panels by fibre optic sensors

Author keywords

[No Author keywords available]

Indexed keywords

BUCKLING; FIBER BRAGG GRATINGS; FIBER OPTIC SENSORS; STRAIN MEASUREMENT; STRUCTURAL ANALYSIS; STRUCTURAL PANELS; TENSILE TESTING;

AIRCRAFT SKIN PANELS;

AIRCRAFT;

EID: 0035360398 PISSN: 09641726 EISSN: None Source Type: Journal
DOI: 10.1088/0964-1726/10/3/310 Document Type: Article

Times cited : (51)

References (8)

1
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- Test results for prediction of composite stresses at skin-stiffener interface
- (1993) ICCM/9 , vol.6 , pp. 722-727
- De Nicolas, F.¹ Huertas García, M.²

2
- 0004632743
- Compression after impact (CAI) behaviour of CF/PIXA stiffened panels for HSCT empennage
- paper no 349
- (1999) ICCM/12, Proc. Int. Conf. on Composite Materials
- Ishikawa, T.¹ Matsushima, M.² Keng Goy Lim, E.³ Hayashi, Y.⁴ Scott, M.L.⁵

3
- 0003201649
- Postbuckling failure of a blade-stiffened carbon-epoxy compression panel
- paper no 188
- (1999) ICCM/12, Proc. Int. Conf. on Composite Materials
- Falzon, B.G.¹ Stevens, K.A.² Goia, M.³ Davies, G.A.O.⁴

4
- 0001277406
- Tooling with reinforced elastomeric materials
- (1992) Compos. Manufact. , vol.3 , pp. 101-111
- Musch, G.¹ Bishop, W.²

5
- 0004586151
- Tooling with reinforced elastomeric materials
- Oxford: Elsevier
- (1992) Composites Tooling Proc. , pp. 90-108
- Musch, G.¹ Bishop, W.²

6
- 0004620520
- AIRTECH International, 2542 East del amo boulevard, PO Box 6207, Carson, CA 90749-6207, USA
- (1992) Manufacturer Information

7
- 0032689424
- Termination and connection methods for optical fibers embedded in aerospace composite components
- (1999) Smart Mater. Struct. , vol.8 , pp. 269-273
- Green, A.K.¹ Shafir, E.²

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.