Background - A joint program (FAA): Honeywell-U.S. Air Force- NASA to develop highly-loaded LPT stages Objective of current work - Application and evaluation of a High-Fidelity numerical simulation for flow field in a highly loaded LPT stage. 1. loss generation mechanism. 2. Reynolds number effects on stage performance
Aerodynamic Loss Generation in a Low-Pressure Turbine Stage with High Lift Blading
2022
31 pages
Report
Keine Angabe
Englisch
Engineering Index Backfile | 1948
|The Application of Ultra High Lift Blading in the BR715 LP Turbine
Online Contents | 2002
|Aerodynamic Inverse Design for Viscous Flow in Turbomachinery Blading
Online Contents | 2007
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