Effect of ply thickness and crack tip damage on failure of notched composite laminates

Effect of ply thickness and crack tip damage on failure of notched composite laminates

Author(s):

Vaidya, Rajesh S. ( Purdue University, West Lafayette, IN )
Klug, J.C. ( Purdue University, West Lafayette, IN )
Sun, C.T. ( Purdue University, West Lafayette, IN )

Publication title:

A collection of technical papers : 38th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit and AIAA/ASME/AHS Adaptive Structures Forum, April 7-10, 1997, Kissimmee, FL

Title of ser.:

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

Ser. no.:

CP973

Pub. Year:

1997

Vol.:

pt. 3

No.:

97-1184

Paper no.:

AIAA-97-1184

Page(from):

2224

Page(to):

2237

Pub. info.:

Reston, Va: American Institute of Aeronautics and Astronautics

ISBN:

9781563472275 [1563472279]

Language:

English

Call no.:

(pt.1)A07400/970595,(pt.2)A07400/970596,(pt.3)A07400/970597,(pt.4)A07400/970598

Type:

Technical Paper

Details

TDL ID:	ZA00006871
Series ID:	PA00000154
Conf. info. (Name):	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit and AIAA/ASME/AHS Adaptive Structures Forum
Conf. info. (Number):	38th
Conf. info. (Venue):	Kissimmee, FL
Conf. info. (Date):	1997.04.07-1997.04.10

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