Using morphological analysis to tackle uncertainty at the design phase for a safety critical application
The gas turbine engine internal air system provides cooling and sealing air to a series of critical subsystems and components such as high pressure gas turbine blades, as well as controlling the thrust load on the turbine and compressor spool assembly. Many potential variations for the internal air...
Main Authors: | P.R.N. Childs, B. Garvey |
---|---|
Format: | Article |
Language: | English |
Published: |
Elsevier
2015-03-01
|
Series: | Propulsion and Power Research |
Subjects: | |
Online Access: | http://www.sciencedirect.com/science/article/pii/S2212540X15000206 |
Similar Items
-
Parametric Investigation of the Combustor-Turbine Interface Leakage Geometry
by: Knost, Daniel G.
Published: (2014) -
A CFD Analysis towards Flow Characteristics of three Pre-swirler Designs
by: Dulac, Adrien
Published: (2012) -
Design Point Performance and Optimization of Humid Air Turbine Power Plants
by: Giovanni D. Brighenti, et al.
Published: (2017-04-01) -
The Optimal Operation Criteria for a Gas Turbine Cogeneration System
by: Atsushi Akisawa, et al.
Published: (2009-04-01) -
Design, Numerical Simulation and Experimental Investigation of Radial Inflow Micro Gas Turbine
by: S. P. Shah, et al.
Published: (2019-01-01)