Fatigue of Aircraft Structures > 2011 > Iss. 3 > 112--133
Source
Abstract
Identifiers
Authors
Keywords
Additional information
Publisher
Fields of science
Bibliography
-
[1] US Patents 2575710 (1951), 3058339 (1962), 3467358 (1969), 3597963 (1971), 4153388 (1979), 4593566 (1986), 4827435 (1989), 5148711 (1992), 5479826 (1996), 6094989 (2000)
-
[2] Witos, M. (1994). Diagnosing of technical condition of turbine engine compressor blades using non-contact vibration measuring method. Dissertation, ITWL Warszawa (pol.)
-
[3] von Flotow A., Drumm, M. J. (2002). Engine Sensing Technology Hardware & Software to Monitor Engine Rotor Dynamics Using Blade Time-Of-Arrival and Tip Clearance. Hood River, OR, USA, www.hoodtech.com