Blank Cover Image

SUBLAMINATE ANALYSIS OF INTERLAMINAR FARCTURE IN COMPOSITES Final Technical

著者名:
Armanios, E.A. ( Georgia Inst. of Tech. )  
掲載資料名:
NASA Technical Reports
発行年:
1986
号:
NASA-CR-177228
通号:
G3/24 43394
パート:
NAS1.26:177228
ペーパー番号:
N86-28130
開始ページ:
1
終了ページ:
89
総ページ数:
89
出版情報:
National Aeronautics and Space Administration
言語:
英語
資料種別:
テクニカルペーパー

類似資料:

1 テクニカルペーパー ANALYSIS OF INTERLAMINAR FRACTURE IN COMPOSITES UNDER COMBINED LOADING Semiannual Report, 12 Aug. 1988 - 11 Feb. 1989

Armanios, Erian A.

National Aeronautics and Space Administration
7 テクニカルペーパー A Sublaminate Model for Creep Buckling Analysis of Thick-Section FRP Composite Structures

Muliana, A., Haj-Ali, R.

American Institute of Aeronautics and Astronautics
2 テクニカルペーパー ANALYSIS OF DELAMINATION RELATED FRACTURE PROCESSES IN COMPOSITES Final Report, 12 Feb. 1986 - 30 Sep. 1988

Armanios, EriaN A.

National Aeronautics and Space Administration
8 テクニカルペーパー Design, Manufacturing and Testing of Elastically Tailored Composite Star Beam Configurations

Kim, I., Dancila, S., Armanios, E.

American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Simple Boundary Element Analysis of Laminated Composite Structures

Makeev,A., Armanios,E.

American Institute of Aeronautics and Astronautics
9 テクニカルペーパー APPROXIMATE ANALYSIS FOR INTERLAMINAR STRESSES IN COMPOSITE STRUCTURES WITH THICKNESS DISCONTINUITIES

Rose, Cheryl A., Starnes, James H., Jr.

National Aeronautics and Space Adminstration
4 テクニカルペーパー ANALYSIS OF DELAMINATION RELATED FRACTURES PROCESSES IN COMPOSITES

Armanios, Erian A.

National Aeronautics and Space Adminstration
10 テクニカルペーパー Approximate analysis for interlaminar stresses in composite structures with thickness discontinuities

Rose, Cheryl A., Starnes, James H., Jr.

American Institute of Aeronautics and Astronautics
5 テクニカルペーパー ANALYSIS OF DELAMINATION REALTED FRACTURE PROCESSES IN COMPOSITES

Armanios, Erian A.

National Aeronautics and Space Adminstration
11 テクニカルペーパー Damage Assessment of Co-cured Composite Joint Strength Under Quasi-static and Fatigue Loading

X. Tan, E. Armanios

American Institute of Aeronautics and Astronautics
6 テクニカルペーパー STRAIN ENERGY RELEASE RATES OF COMPOSITE INTERLAMINAR END-NOTCH AND MIXED-MODE FRACTURE: A SUBLAMINATE/PLYLEVEL

Valisetty, R. R.

National Aeronautics and Space Administration
12 テクニカルペーパー Composite Processing Development to Improve Interlaminar Strength Using Ply Interface Particles (Center Director's Discretionary Fund Final REport No. 93-13)

Nett3es, A.T.

National Aeronautics and Space Adminstration
1
 
2
 
3
 
4
 
5
 
6
 
7
 
8
 
9
 
10
 
11
 
12