The Ultrasonic Testing of B.66 Compressor Blades
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 October 1963
Abstract
A Description of the Technique and Equipment used successfully to carry out Ultrasonic Inspection of Compressor Rotor Blades of the Allison J.7I Turbojet following the loss of a number of Douglas B.66 Bomber Aircraft of the United States Air Force in Europe due to Engine failure
Citation
Harris‐Maddox, B. (1963), "The Ultrasonic Testing of B.66 Compressor Blades", Aircraft Engineering and Aerospace Technology, Vol. 35 No. 10, pp. 293-296. https://doi.org/10.1108/eb033791
Publisher
:MCB UP Ltd
Copyright © 1963, MCB UP Limited