Skip to Main Content
Keywords: Reliability management
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 (2008) 80 (5): 516–525.
Published: 05 September 2008
... are on the same high‐pressure shaft (N2) that operates at high speed. © Emerald Group Publishing Limited 2008 Aircraft engines Condition monitoring Fuzzy logic Maintenance Reliability management Commercial aircraft Aircraft maintenance implies actions that restore an item...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2006) 78 (3): 226–235.
Published: 01 May 2006
... 2415 was adopted for the main wing, and NACA 0012 was adopted for the tail plane. Among these profiles under consideration there were: Aeroplanes Aerodynamics Reliability management For details see Figures 10‐13 . airworthiness regulations (FAR, JAR); air traffic control...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2006) 78 (3): 204–210.
Published: 01 May 2006
...). The following equation shows the pressure loss estimation (ESDU 66027, 1966). Equation 1 where, ∑K=summation of considered components' loss coefficients. © Emerald Group Publishing Limited 2006 Aeroplanes Fuel consumption Reliability management Component manufacturing Fault tolerance...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2005) 77 (6): 478–485.
Published: 01 December 2005
... approach. This method would have more pronounced effects in aircraft types with behaviors between commercial and training (for example, amphibious aircraft). © Emerald Group Publishing Limited 2005 Reliability management Aircraft Design Structural design Within the random variables...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2005) 77 (2): 148–151.
Published: 01 April 2005
... life of aircraft structures. The calculated optimal stress distribution function can be used with commercial reliability software to estimate the crack size population. © Emerald Group Publishing Limited 2005 Design Reliability management Aerospace industry We develop Yang's...

or Create an Account

Close Modal
Close Modal