|
This article is cited in 2 scientific papers (total in 2 papers)
MECHANICS
An optimal design technology for aerodynamic configurations based on the numerical solutions of the full Navier–Stokes equations
S. V. Peygina, K. A. Stepanovab, S. V. Timchenkoba a Innovation
Center "SKOLKOVO", Moscow, Russian Federation
b Tomsk State University, Tomsk, Russian Federation
Abstract:
A new approach for optimization of essentially 3D aerodynamic shapes intended to minimize
their drag is proposed. The method allows one to apply the non-linear surfaces, which are
typically used for the complex aircraft junctions such as wing-to-body fairing. This method
involves the solution of full Navier–Stokes equations for the objective function calculation, and
the optimization technology is based on the genetic algorithms. The important features of the
method are both the ability to take into account the multiple geometrical and aerodynamic
constraints and the high level of computational efficiency achieved by the complex multilevel
parallelization and reduced-order modeling approach. This method was applied for a wing-tobody
fairing optimization on a typical medium-range aircraft at the realistic transonic flight
conditions.
The constraint handling can be described as follows: it is proposed to employ the search paths
through both feasible and infeasible points instead of a traditional approach where only feasible
points can be included in a path. For this purpose, the search space is extended by evaluating
points (in terms of fitness) which do not satisfy the constraints imposed by optimization problem.
The required extension of an objective function can be implemented due to a basic property of
genetic algorithms: they are not confined to only smooth solutions in contrast to the classical
optimization methods.
The results demonstrate that the proposed approach provides a significant drag reduction and
is applicable for engineering and designing.
Keywords:
optimal design, full Navier–Stokes equations, non-linear constraints, drag coefficient, pitch moment.
Received: 10.11.2017
Citation:
S. V. Peygin, K. A. Stepanov, S. V. Timchenko, “An optimal design technology for aerodynamic configurations based on the numerical solutions of the full Navier–Stokes equations”, Vestn. Tomsk. Gos. Univ. Mat. Mekh., 2017, no. 50, 90–98
Linking options:
https://www.mathnet.ru/eng/vtgu621 https://www.mathnet.ru/eng/vtgu/y2017/i50/p90
|
Statistics & downloads: |
Abstract page: | 128 | Full-text PDF : | 52 | References: | 20 |
|