Cylindrical, stand-alone tubes of plasma-sprayed alumina were tested in com
pression in the axial direction at room temperature, using strain gauges to
monitor axial and circumferential strains. The primary compression-loading
profile used was cyclic loading, with monotonically increased peak stresse
s. Hysteresis was observed in the stress-strain response on unloading, begi
nning at a peak stress of 50 MPa. The modulus decreased as the maximum appl
ied stress increased. The stress-strain response was only linear at low str
esses; the degree of nonlinearity at high stresses scaled with the stress a
pplied. One-hour dwells at constant stress at room temperature revealed a t
ime-dependent strain response. Using transmission electron microscopy and a
coustic emission to investigate deformation mechanisms, the stress-strain r
esponse was correlated with crack pop in, growth, and arrest. It is propose
d that the numerous defects in plasma-sprayed coatings, including porosity
and microcracks, serve as sites for crack nucleation and/or propagation. As
these small, nucleated cracks extend under the applied stress, they propag
ate nearly parallel to the loading direction along interlamellae boundaries
. With increasing stress, these cracks ultimately link, resulting in catast
rophic failure.