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Propulsion systems in future
hypersonic vehicles will require use of actively cooled structures that can
withstand extreme thermomechanical loads. Candidate designs and materials
for such structures have previously been identified through conventional
yield-based design principles. The present article outlines an approach that utilizes
concepts of localized plasticity and shakedown under cyclic loading in the
design process. For this purpose, an established computational technique is
used to determine shakedown limits for prototypical cooled structures. The
results are employed in a design sensitivity study. The study demonstrates
that, by allowing for shakedown, structures with areal densities significantly
lower than those obtained from yield-limited design can be obtained. The
magnitude of the benefits depends on the specific geometry of interest, the
thermomechanical boundary conditions and the constraints placed on the
design.
Department of Mechanical and
Aerospace Engineering and Department of Chemical Engineering
and Materials Science
University of California
Irvine, CA 92697-3975
United States