Microcracking of Symmetric Cross-ply Laminates Subjected to Biaxial Loading

Microcracking of Symmetric Cross-ply Laminates Subjected to Biaxial Loading

著者名:

Bapanapalli, S. ( University of Florida, Gainesville, FL )
Sankar, B.
Primas, R. ( Boeing-Rocketdyne, Canoga Park, CA )

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

シリーズ巻号:

46th

発行年:

2005

通号:

2005-2230

ペーパー番号:

AIAA Paper 2005-2230

出版情報:

[Reston, Va.]: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200506 [CD-ROM 2005 Disc 6]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001621
シリーズID:	PA00000154
会議名:	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
回次:	46th
会議開催地:	Austin, Texas
会議開催年:	2005.04.18-2005.04.21

類似資料:

1 テクニカルペーパー Parametric investigation of gas permeability in cross-ply composite laminates using three-dimensional finite elements J. Xu, B. Sankar American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Buckling Behavior of Long Symmetrically Laminated Plates Subjected to Combinal Loadings Nemeth, Michael P. National Aeronautics and Space Adminstration
2 テクニカルペーパー Comparison of Materials for Integrated Thermal Protection Systems for Spacecraft Reentry C. Gogu, S. Bapanapalli, R. Haftka, B. Sankar American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Wave propagation in a multilayered laminated cross-ply composite plate Karunasena, W., Shah, A. H., Datta, S. K. The American Society of Mechanical Engineers
3 テクニカルペーパー Micromechanical Analysis of Composite Truss-Core Sandwich Panels for Integral Thermal Protection Systems O. Martinez, S. Bapanapalli, B. Sankar, R. Haftka, M. Blosser American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Bonded joints of unidirectional and cross-PLY laminates: an experimental study Roy, A.K., Donaldson, S.L., Shoeppner, G.A. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー (Student Paper) Analysis and Design of Corrugated-Core Sandwich Panels for Thermal Protection Systems of Space Vehicles S. Bapanapalli, O. Martinez, C. Gogu, B. Sankar, R. Haftka, M. Blosser American Institute of Aeronautics and Astronautics	10 テクニカルペーパー EFFECT OF ADHESIVE INTERLEAVING AND DISCONTINUOUS PLIES ON FAILURE OF COMPOSITE LAMINATES SUBJECT TO TRANSVERSE NORMAL LOADS Jegley, Dawn C. National Aeronautics and Space Administration
5 テクニカルペーパー Microcracking in composite laminates under thermal and mechanical loading Maddocks, Jason R. National Aeronautics and Space Adminstration	11 テクニカルペーパー Reliability of Laminated Composite Beams Subjected to Subtangential Loads Goyal, V., Kapania, R. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Prediction of microcracking in composite laminates under thermomechanical loading Maddocks, Jason R., Mcmanus, Hugh L. National Aeronautics and Space Adminstration	12 テクニカルペーパー Experimental Observation of Microcracking of Composite Laminates Under Cryogenic Temperature Kim, R., Donaldson, S. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12