Stability Analysis of Unstarted Supersonic Cascade Flows by Actuator Disk Method

2000 ◽  
Vol 2000.4 (0) ◽  
pp. 61-62
Author(s):  
Kimihiko MITSUDA ◽  
Yukiharu IWAMOTO ◽  
Kazuhiko YOKOTA ◽  
Yoshinobu TSUJIMOTO
Keyword(s):  
Stability Analysis ◽  
Actuator Disk ◽  
Disk Method

scholarly journals CFD and Experimental Studies on Wind Turbines in Complex Terrain by Improved Actuator Disk Method

2017 ◽  
Vol 854 ◽  
pp. 012028 ◽  
Author(s):  
Xin Liu ◽  
Shu Yan ◽  
Yanfei Mu ◽  
Xinming Chen ◽  
Shaoping Shi
Keyword(s):  
Wind Turbines ◽  
Complex Terrain ◽  
Experimental Studies ◽  
Actuator Disk ◽  
Disk Method

An actuator disk method with tip-loss correction based on local effective upstream velocities

Wind Energy ◽  
2018 ◽  
Vol 21 (9) ◽  
pp. 766-782 ◽  
Author(s):  
Maud Moens ◽  
Matthieu Duponcheel ◽  
Grégoire Winckelmans ◽  
Philippe Chatelain
Keyword(s):  
Actuator Disk ◽  
Disk Method

Linearized Solutions for the Supersonic Flow Through Turbomachinery Blade Rows (Using Actuator Disk Theory)

1980 ◽  
Vol 102 (3) ◽  
pp. 330-337
Author(s):  
J. H. Horlock ◽  
C. F. Grainger
Keyword(s):  
Supersonic Flow ◽  
Method Of Characteristics ◽  
Three Dimensional ◽  
Actuator Disk ◽  
Blade Row ◽  
Flow Through ◽  
Twisted Blade ◽  
Disk Method

An actuator disk method is developed for calculating the flow through the blade rows of a turbomachine in which the velocity relative to the blading may be supersonic. The method is compared with calculations of the fully supersonic flow through a twisted blade row using a three-dimensional method of characteristics.

Assessment of blade element actuator disk method for simulations of ducted tidal turbines

2020 ◽  
Vol 154 ◽  
pp. 290-304
Author(s):  
F. Baratchi ◽  
T.L. Jeans ◽  
A.G. Gerber
Keyword(s):  
Actuator Disk ◽  
Tidal Turbines ◽  
Disk Method ◽  
Blade Element
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