The work reported is part of a program on flaw detection in turbine rotor components. The goal is to image or map non-surface breaking fatigue cracks near the bore hole surface of an aircraft engine disk with the aid of ultrasonic inversion techniques. Presented are results of inversion of both pitch-catch and pulse-echo data with the inversion technique discussed in detail in the companion paper.
|Original language||English (US)|
|Title of host publication||Review of Progress in Quantitative Nondestructive Evaluation|
|Editors||Donald O. Thompson, Dale E. Chimenti|
|Number of pages||10|
|Publication status||Published - Dec 1 1984|
|Name||Review of Progress in Quantitative Nondestructive Evaluation|
All Science Journal Classification (ASJC) codes