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Thermal Testing of Tow-Placed, Variable Stiffness PanelsCommercial systems for precise placement of pre-preg composite tows are enabling technology that allows fabrication of advanced composite structures in which the tows may be precisely laid down along curvilinear paths within a given ply. For laminates with curvilinear tow paths, the fiber orientation angle varies continuously throughout the laminate, and is not required to be straight and parallel in each ply as in conventional composite laminates. Hence, the stiffness properties vary as a function of location in the laminate, and the associated composite structure is called a "variable stiffness" composite structure.
Document ID
20010039508
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Wu, K. Chauncey
(NASA Langley Research Center Hampton, VA United States)
Guerdal, Zafer
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Structural Mechanics
Report/Patent Number
AIAA Paper 2001-1190
Report Number: AIAA Paper 2001-1190
Meeting Information
Meeting: 42nd Structures, Structural Dynamics and Materials Conference and Exhibit
Location: Seattle, WA
Country: United States
Start Date: April 16, 2001
End Date: April 19, 2001
Sponsors: American Inst. of Aeronautics and Astronautics, American Society of Civil Engineers, American Society for Composites, American Helicopter Society, Inc., American Society of Mechanical Engineers
Distribution Limits
Public
Copyright
Public Use Permitted.
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