Boundary Velocity Suboptimal Control of Incompressible Flow in Cylindrically Perforated Domains

Author(s):  
Peter I. Kogut ◽  
Günter R. Leugering

2009 ◽  
Vol 11 (2) ◽  
pp. 283-314
Author(s):  
Ciro D’Apice ◽  
◽  
Umberto De Maio ◽  
Peter I. Kogut ◽  
◽  
...  


1992 ◽  
Vol 30 (1) ◽  
pp. 167-181 ◽  
Author(s):  
Max D. Gunzburger ◽  
Lisheng Hou ◽  
Thomas P. Svobodny






AIAA Journal ◽  
1997 ◽  
Vol 35 ◽  
pp. 585-586
Author(s):  
P. A. Russell ◽  
S. Abdallah


Author(s):  
MARA NILZA ESTANISLAU REIS ◽  
Wender Oliveira ◽  
Pedro Américo Almeida Magalhães Júnior






Author(s):  
Marcel Escudier

This chapter is concerned primarily with the flow of a compressible fluid through stationary and moving blading, for the most part using the analysis introduced in Chapter 11. The principles of dimensional analysis are applied to determine the appropriate non-dimensional parameters to characterise the performance of a turbomachine. The analysis of incompressible flow through a linear cascade of aerofoil-like blades is followed by the analysis of compressible flow. Velocity triangles for flow relative to blades, and Euler’s turbomachinery equation, are introduced to analyse flow through a rotor. The concepts introduced are applied to the analysis of an axial-turbomachine stage comprising a stator and a rotor, which applies to either a compressor or a turbine.



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