Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Anthony Haslam"'
The paper presents a methodology for the numerical design and optimization of a distortion-free two-dimensional Mach 2.5 nozzle based on a parametric model. The non-uniformities generated at the Mach wave reflections downstream of the nozzle throat t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9dbbfce662bce43fffcfe52c68ecb454
https://dspace.lib.cranfield.ac.uk/handle/1826/19288
https://dspace.lib.cranfield.ac.uk/handle/1826/19288
Publikováno v:
Open Engineering, Vol 5, Iss 1 (2015)
This paper provides a tool for the estimation of the operational severity of a high pressure turbine blade of an aero engine. A multidisciplinary approach using aircraft/ engine performance models which provide inputs to a thermo-mechanical fatigue d
The Influence of Humidity on the Creep Life of a High Pressure Gas Turbine Blade: Part II—Case Study
Publikováno v:
Volume 3: Cycle Innovations; Education; Electric Power; Fans and Blowers; Industrial and Cogeneration.
The determination of the rate of heat transfer from the turbine blade in a cross flow is important in hot section gas turbine life assessment. For design purposes, the rate of heat transfer is normally fixed by semi-empirical correlations. These corr
Publikováno v:
Volume 3: Cycle Innovations; Education; Electric Power; Fans and Blowers; Industrial and Cogeneration.
The cooling of high temperature gas turbines has been the subject of intensive work over the past few decades. Analysis of the metal temperature of cooled blades requires the solution of the equations governing the heat flow through the blade given t