Investigations of Unsteady Film Cooling Performance on Rotor Squealer Tip
JOURNAL- XIAN JIAOTONG UNIVERSITY ; 44 , 5 ; 5-9
01.01.2010
5 pages
Aufsatz (Zeitschrift)
Unbekannt
DDC: | 500 |
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Effect of squealer tip geometry on rotor blade aerodynamic performance
Online Contents | 2013
|Effect of Pressure Side Winglet on Film Cooling and Heat Transfer Performance of Blade Squealer Tip
British Library Online Contents | 2017
|Film-Cooling Effectiveness on Squealer Cavity and Rim Walls of Gas-Turbine Blade Tip
Online Contents | 2006
|