Critical and coincidence frequencies of panels are important in studyi
ng their behaviour under acoustic excitation. Most spacecraft structur
al panels are of honeycomb sandwich construction and many of them have
face sheets made of composite material. The critical and coincidence
frequencies of such panels an discussed here. Expressions for critical
and coincidence frequencies of thick isotropic and thin as well as th
ick symmetric composite panels are derived. It is shown that the ortho
tropic behaviour and transverse shear flexibility of the panels affect
s the critical and coincidence frequencies. The critical frequency of
a typical composite honeycomb sandwich panel obtained using the above
expressions match well with experimental results. (C) 1997 Academic Pr
ess Limited.