In the magnetic recording head gimbal assembly, the ceramic slider is attac
hed to the stainless-steel flexure of the suspension by a thin layer of adh
esive. The mismatch of the thermal expansion coefficients between the stain
less steel and the ceramic causes thermal bending, or crown sensitivity, as
a result of temperature variation. Crown sensitivity is a measure of crown
change with temperature. The crown plays a critical role in the flying att
itude of the slider as well as interface tribology. For a viscoelastic adhe
sive, both time and temperature are coupled during the evolution of the cro
wn. We develop a viscoelastic solution for slider deflection based on our p
reviously derived elastic analysis. The elastic-viscoelastic correspondence
principal and Laplace transformation techniques are employed to extend the
elastic solution to the viscoelastic regime. The experimentally measured v
iscoelastic master curve and time-temperature shift factors define the adhe
sive properties. The model calculation provides the deflection of the bonde
d assembly for an arbitrary thermal history. The calculated deflection is c
ompared with test results using several adhesives with different viscoelast
ic properties. Our results are in qualitatively good agreement with the mea
sured slider crown sensitivity.