Several NDE techniques are available for detecting the symptoms of corrosio
n such as pillowing, disbonding and metal loss. However, on real aircraft,
each of these symptoms may not be caused by corrosion, For example, trapped
swarf can cause pillowing, sealant layers may never have been bonded, and
metal can have been removed at the construction stage, or during a repair,
sometimes without adequate documentation to inform the NDE inspector Instan
ces of all of these have been found in VC10 aircraft in a recent teardown e
xercise. A method that measures the roughness of a hidden surface could pro
vide that necessary confirmation that a disbond or region of thinning is ac
tually corroded This paper describes the development and evaluation of a te
chnique which uses the frequency-dependence of the reflection coefficient a
t a rough interface to measure the surface roughness. Several other workers
have reported methods for determining top-surface roughness but hidden sur
faces present many more complications, which are the subject of this paper:
Hidden surfaces roughnesses from 5 mum to 40 mum can he measured with an a
ccuracy of +/- 5 mum. The method can be applied to full-waveform data files
, or in real-time whilst scanning, using the ANDSCAN(R) system. The depende
nce of the method on analysis parameters, stand-off media and ultrasonic co
nfiguration is also discussed.