Skip to Main Content
Keywords: Fault analysis
Close
Follow your search
Access your saved searches in your account

Would you like to receive an alert when new items match your search?
Close Modal
Sort by
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2003) 75 (1): 27–32.
Published: 01 February 2003
... of the unit. The approaches only require a database of historical data, and the models are easily and quickly built from these. They can also easily handle very large problems (Yoon and MacGregor, 2001). Fault analysis Aircraft In terms of the concept of fault diagnosis, aircraft...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2003) 75 (1): 11–17.
Published: 01 February 2003
... by the conventional triangulation method. This is a promising method for non‐destructive testing by AE method of aircraft frame structures. © MCB UP Limited 2003 Non‐destructive testing Defects Fault analysis Acoustic emission (AE) pertains to non‐destructive testing methods and is used to locate...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2002) 74 (1): 4–8.
Published: 01 February 2002
... to time‐delay estimation of two independent continuous AE sources on an aluminum beam. It is shown that it is possible to estimate time delays by ICA, and thus to locate two independent simultaneously emitted sources. © MCB UP Limited 2002 Aluminum Defects Fault analysis A common goal...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2000) 72 (3): 258–261.
Published: 01 June 2000
... and feathering spring in servo piston. The Y12(IV) aircraft received the FAA airworthiness certificate and manufacture certificate in July 1995. Propellers Pitch Fault analysis © MCB UP Limited 2000 ...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2000) 72 (2): 142–155.
Published: 01 April 2000
... the effects of angle of twist, rotational speed and laminate configuration. © MCB UP Limited 2000 Finite element Fault analysis Plates Shear degradation E1, E2 Young’s moduli of a lamina along (1) and transverse (2)to the fibre direction...

or Create an Account

Close Modal
Close Modal