3 edition of High strain rate properties of off-axis composite laminates. found in the catalog.
High strain rate properties of off-axis composite laminates.
Isaac M. Daniel
1991 by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, DC], [Springfield, Va .
Written in English
|Series||NASA contractor report -- 189084., NASA contractor report -- NASA CR-189084.|
|Contributions||United States. National Aeronautics and Space Administration.|
|The Physical Object|
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Get this from a library. High strain rate properties of off-axis composite laminates. Part II: final report. [I M Daniel; United States. National Aeronautics and Space Administration.]. Studies are presented on in-plane shear properties of a typical plain weave E-glass/epoxy composite under high strain rate loading.
In-plane shear properties were determined with ±45 degree off. Hosur et al. [13,14] investigated variations of dynamic strength and stiffness of the woven carbon/epoxy composite laminates under high strain rate out-of-plane (throughthe-thickness) compressive.
for a wide range of uses, when allowance is made for poor off-axis properties. (The density of these materials can be calculated by applying the Law of Mixtures, using data from Tables and.