Unsteady viscous compressible flow through a straight channel with porous walls in the presence of magnetic field and its solution

1974 ◽  
Vol 22 (1) ◽  
pp. 13-21
Author(s):  
R. S. L. Srivastava ◽  
L. M. Srivastava
Keyword(s):  
Magnetic Field ◽  
Compressible Flow ◽  
Straight Channel ◽  
Flow Through ◽  
Porous Walls ◽  
Viscous Compressible Flow

Viscous Compressible Flow Through a Hole in a Plate, Including Entry Effects

2002 ◽  
Vol 39 (3) ◽  
pp. 516-518 ◽  
Author(s):  
P. M. Galluzzo ◽  
H. Babinsky ◽  
G. R. Inger
Keyword(s):  
Compressible Flow ◽  
Flow Through ◽  
Viscous Compressible Flow

Parallelizable block diagonal preconditioners for 3D viscous compressible flow calculations

1993 ◽  
Author(s):  
LAURA DUTTO ◽  
WAGDI HABASHI ◽  
MICHEL FORTIN ◽  
MICHEL ROBICHAUD
Keyword(s):  
Compressible Flow ◽  
Viscous Compressible Flow ◽  
Block Diagonal

Flow through axial-flow-turbomachinery blading

2018 ◽  
Author(s):  
Marcel Escudier
Keyword(s):  
Flow Velocity ◽  
Compressible Flow ◽  
Dimensional Analysis ◽  
Incompressible Flow ◽  
Compressible Fluid ◽  
Axial Flow ◽  
Linear Cascade ◽  
Dimensional Parameters ◽  
Flow Through

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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