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Plate Deformation Behavior of Polymer Matrix Composite-Ti Honeycomb-Metal Sandwiches for Pressurized Propulsion Component ApplicationsTHe objectives are: 1. To experimentally validate bi-axial plate flexural performance of PMC-Ti H/C-A286 sandwich panels for the internally pressurized RBCC combustion chamber support structure. 2. To explore ASTM 2-D plate flexure test (D 6416) to simulate the internal pressure loading and to correlate the results with analytical and FE modeling based on 2-D flexure properties.
Document ID
20040086941
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Bertelsen, William D. (Bertelsen Mfg. Co., Inc. Neponset, IL, United States)
Shin, E. eugene (NASA Glenn Research Center Cleveland, OH, United States)
Thesken, John C. (NASA Glenn Research Center Cleveland, OH, United States)
Sutter, James K. (NASA Glenn Research Center Cleveland, OH, United States)
Martin, Rich (NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Composite Materials
Meeting Information
Meeting: Joint Meetings of ASTM D30 Committee, Composite Materials Hand Book (MIL-HDBK-17)
Location: Charleston, SC
Country: United States
Start Date: October 27, 2003
End Date: October 31, 2003
Sponsors: American Society of Tool and Mfg. Engineers
Funding Number(s)
OTHER: 708-31-16
Distribution Limits
Public
Copyright
Public Use Permitted.

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