Previous investigations have used Hankel transforms to establish the amplit
udes of the wave fields resulting from arbitrary angle impingement on a cir
cular orifice in a baffle. Investigations have also been undertaken on the
effects of model coupling between the higher modes in the orifice. In parti
cular, these studies concentrated on establishing the contributions at the
cut-on wave number for a particular mode. This work is extended to introduc
e a method of simply approximating the complex amplitude of the forward and
backward waves in the duct at the cut-on wave number, based only on the mo
dal wave number. The interest focuses on the cut-on wave number because the
forcing functions for the various fields will be at a maximum at cut-on. T
his technique is established by observing the relationships between the pea
k values of the driving functions and the modal wave number. If simple appr
oximations are established for the in-duct field, it is also possible to ap
proximate the maximum amplitude of the scattered field. (C) 2001 Acoustical
Society of America.