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Cryogenic Mixed Mode I – Mode II Fracture Toughness of Various Polymer Composite MaterialsThe present study investigates the mixed mode interlaminar fracture toughness of six polymer matrix composite materials at both room temperature and cryogenic liquid nitrogen temperature. The single leg bending test employed gives a mix of Mode I (opening) and Mode II (in-plane shearing) cracking. The tested thermoplastic-matrix composites were shown to have total mixed mode toughnesses 3.1–4.3 times higher than those of representative thermoset resin composites.
Document ID
20260005315
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Nguyet Nhi Nguyen
(NASA Intern Hampton, Virginia, United States)
Jin Ho Kang
(Langley Research Center Hampton, United States)
William Johnston
(Langley Research Center Hampton, United States)
Benjamin Jensen
(Langley Research Center Hampton, United States)
Jeffrey Hinkley
(Langley Research Center Hampton, United States)
Wilfredo Flores
(Langley Research Center Hampton, United States)
James Ratcliffe
(Langley Research Center Hampton, United States)
Laurence Thomsen
(Langley Research Center Hampton, United States)
Date Acquired
June 11, 2026
Publication Date
June 1, 2026
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Composite Materials
Nonmetallic Materials
Report/Patent Number
NASA/TM-20260005315
Funding Number(s)
WBS: 295670.01.24.23.13
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
Keywords
Carbon fiber
Cryogenic
Toughness
Fuel Vessel
Thermoset
Thermoplastic
Polymer
Composite
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