Solution of inverse problems of gas dynamics of flat compressor cascades based on numerical simulation of turbulent flows

Abstract

This paper presents a technique for solving inverse problems in gas dynamics of flat compressor cascades, based on a numerical simulation of turbulent flows. This technique is based on the application of quasi-solutions searching method to the solution of inverse problems. In this case the solution of the inverse problem is reduced to solving the problem of finding the global extreme of some target function. A parametric description of the shape of cascade profiles is made using an original method, based on the Bezier curves and the system of Hicks – Henne smooth convex functions. The application of this method makes it possible to vary the geometric parameters of the cascade in wide ranges by means of a relatively small number of variable parameters and the preservation of the physically feasible profile path. The calculation of the target function is performed by simulating the flow from the numerical integration of the averaged Navier–Stokes equations which are closed by means of the Spalart–Allmaras one-parameter turbulence model. A hybrid genetic algorithm is used to find the extreme of the target function. The technique proposed allows the determination of the geometrical parameters of the cascade for a given pressure distribution on the contour of the desired profile as well as from given integral aerodynamic characteristics of the cascade. It can also be used to solve problems of aerodynamic optimization of compressor cascades. In addition, this technique can be easily adapted to the solution of similar problems in the three-dimensional formulation.

Authors and Affiliations

S. Melashich

Keywords

Related Articles

Experimental Investigations of Multiblade Wind Wheel Model

The majority of the existing techniques for studying the characteristics of physical models of wind genera-tors are oriented on the use of the specialized equipment and a wind tunnel. In some cases, these investigations...

Development and full-scale tests of sound suppressors for small arms with spherical baffles

The paper presents information about sound suppressors for small arms using spherical baffles. Data on patented products of this type are reported, beginning in 1910, when the sound suppressor design with such basic esse...

. On the aerodynamic optimization of impellers of supersonic compressor stages.

The study deals with the pressing problem of diminution in the computer time for an aerodynamic optimization of blade rims of axial compressors when a numerical simulation of the flow based on the full averaged Navier-St...

Numerical simulation of supersonic flow over Zenit-2SLБ launch vehicle

The results of a numerical simulation of a supersonic flow over the Zenit-2SLБ launch vehicle at angle of attack 5, 15 and 25 degrees are presented. Attention in this work is devoted to obtaining the proved three-dimensi...

On the statement of problem of optimization in design parameters of solid rocket engine

The problem of the optimization the design parameters of the solid rocket engine as a nonlinear mathemati-cal programming problem with equality/inequality constraints is formulated. The elements of a mathematical model o...

Download PDF file
  • EP ID EP355105
  • DOI -
  • Views 81
  • Downloads 0

How To Cite

S. Melashich (2015). Solution of inverse problems of gas dynamics of flat compressor cascades based on numerical simulation of turbulent flows. Технічна механіка, Техническая механика, Technical Mechanics, 1(1), 65-72. https://europub.co.uk/articles/-A-355105