Discussion: “Three-Dimensional Supersonic Flow Through a Cascade of Twisted Flat Plates” (Grainger, C. F., 1980, ASME J. Fluids Eng., 102, pp. 338–343)

1980 ◽  
Vol 102 (4) ◽  
pp. 520-520
Author(s):  
L. H. Smith
Keyword(s):  
Supersonic Flow ◽  
Three Dimensional ◽  
Flat Plates ◽  
Flow Through

Three Dimensional Supersonic Flow Through a Cascade of Twisted Flat Plates

1980 ◽  
Vol 102 (3) ◽  
pp. 338-343
Author(s):  
C. F. Grainger
Keyword(s):  
Method Of Characteristics ◽  
Three Dimensional ◽  
Axial Flow ◽  
Finite Difference Approximation ◽  
Difference Approximation ◽  
Flat Plates ◽  
Three Dimensional Flow ◽  
Dimensional Flow ◽  
Two Dimensional Flow ◽  
Flow Through

The three-dimensional flow through a cascade of twisted flat-plate blades is calculated using a computer program based on a finite-difference approximation to the method of characteristics. The relative flow is supersonic but the axial flow is subsonic. For two-dimensional flow under similar conditions, the inlet flow field is one of “unique-incidence,” the effect discussed by Starken (5) and others. The main purpose of the present work is to extend the understanding of this effect to three-dimensional flow. Important differences between the two and three-dimensional flow fields are explained in terms of the interaction between neighboring sections of the flow.

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.

Applicability of Axisymmetric Analysis in Predicting Supersonic Flow Through Annular Cascades

1977 ◽  
Vol 99 (1) ◽  
pp. 115-120
Author(s):  
Hans-Heiner Fruehauf
Keyword(s):  
Supersonic Flow ◽  
Differential Equations ◽  
Three Dimensional ◽  
Supersonic Flows ◽  
Dimensional Model ◽  
Surfaces Of Revolution ◽  
Three Dimensional Model ◽  
Dynamical Parameters ◽  
Flow Through ◽  
Blade Model

Solutions of the differential equations of the axisymmetric model and circumferentially averaged solutions of the differential equations of the three-dimensional model are compared quantitatively for steady supersonic flows through rotating annular cascades. Thereby three-dimensional corrections for flow quantities, which determine the applicability of the axisymmetric analysis, are investigated as a function of geometrical and gas dynamical parameters. Finally, these three-dimensional corrections are compared to three-dimensional corrections for the solutions of the usual blade-to-blade model on cylindrical surfaces of revolution for identical annular cascades.

Spatial Supersonic Flow Through Annular Cascades

1976 ◽  
Vol 98 (2) ◽  
pp. 274-280
Author(s):  
H. H. Fruehauf
Keyword(s):  
Supersonic Flow ◽  
Approximation Method ◽  
Method Of Characteristics ◽  
Three Dimensional ◽  
Dimensional Approximation ◽  
Practical Design ◽  
Dynamical Parameters ◽  
Flow Through ◽  
Guiding Principles

The spatial supersonic flow through rotating and stationary annular cascades is analyzed by means of a nonlinear three-dimensional method of characteristics. Three-dimensional corrections for flow quantities referred to a quasi-three-dimensional approximation method are determined depending on geometric and gas dynamical parameters. Characteristic properties of spatial supersonic flow through annular cascades are analyzed, leading to guiding principles for practical design purposes.

Three-Dimensional Mixing Flow Field in Supersonic Flow Induced by Injected Secondary Flow through a Traverse Circular Nozzle

1995 ◽  
pp. 163-170
Author(s):  
Shigeru Aso ◽  
Shozo Maekawa ◽  
Michiaki Tan-Nou ◽  
Satosh Okuyama ◽  
Yasunori Ando ◽  
...  
Keyword(s):  
Supersonic Flow ◽  
Flow Field ◽  
Secondary Flow ◽  
Three Dimensional ◽  
Circular Nozzle ◽  
Flow Through

scholarly journals Response surface analysis of nozzle parameters at supersonic flow through microjets

2021 ◽  
pp. 1-16
Author(s):  
Turki Al-Khalifah ◽  
Abdul Aabid ◽  
Sher Afghan Khan ◽  
Muhammad Hanafi Bin Azami ◽  
Muneer Baig
Keyword(s):  
Supersonic Flow ◽  
Response Surface ◽  
Surface Analysis ◽  
Response Surface Analysis ◽  
Flow Through
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