Thermal modelling and control of high pressure turbine subsystems
The control and monitoring of aircraft engine subsystems is one of the leading fields of research for improving overall performance. As engine sophistication increases, more sensor information becomes available to the digital control system, as well as options for active flow control technologies. I...
Main Author: | van Paridon, Andrew |
---|---|
Other Authors: | Ireland, Peter T. ; Bacic, Marko |
Published: |
University of Oxford
2016
|
Online Access: | http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728812 |
Similar Items
-
SYNTHESIS OF INTELLECTUAL SUBSYSTEMS OF DYNAMIC DIAGNOSIS OF THE CONDITION OF TURBINE UNITS THERMAL POWER
by: Alibek Suleimenov, et al.
Published: (2017-06-01) -
Thermal management and control of space satellite systems and subsystems in orbit
by: Van Wyk, Peter Arnold
Published: (2012) -
Subsystem eigenstate thermalization hypothesis
by: Dymarsky, Anatoly, et al.
Published: (2018) -
Analysis and Design of the Nano-satellite Thermal Control Subsystem
by: Yin-hui Hsieh, et al.
Published: (2009) -
Design, Analysis and Verification of Thermal Control Subsystem for the CKUTEX Microsatellite
by: Jhan-RueiChang, et al.
Published: (2012)