scholarly journals Compressible Flow Structures Interaction with a Two-Dimensional Ejector: A Cold-Flow Study

2009 ◽  
Vol 25 (3) ◽  
pp. 707-716 ◽  
Author(s):  
H. Zare-Behtash ◽  
K. Kontis
2000 ◽  
Vol 4 (2) ◽  
pp. 125-133 ◽  
Author(s):  
Zoran Dimitrijević ◽  
Guy Daniel Mortchéléwicz ◽  
Fabrice Poirion

Author(s):  
Romuald Rządkowski

A numerical model for the calculation of resonance stationary response of mistuned bladed disc is presented. The bladed disc model includes all important effects on a rotating system of the real geometry. The excitation forces were calculated by a code on the basis of two-dimensional compressible flow (to M < 0.8) for thin airfoil blades. The calculations presented in this paper show that centrifugal stress, and the values of excitation forces, play an important role in considering the influence of mistuning on the response level.


2015 ◽  
Vol 9 (2) ◽  
Author(s):  
Vladimir Evgenyevich Vershinin ◽  
Rodion Mikhaylovich Ganopolsky ◽  
Vitaly Olegovich Polyakov

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