Abstract

Shape optimization in unsteady flow problems enables the consideration of dynamic effects on design. The ability to treat unsteady effects is attractive, as it can provide performance gains when compared to steady-state design methods for a variety of applications in which time-varying flows are of paramount importance. This is the case, for example, in turbomachinery or rotorcraft design. Given the high computational cost involved in time-accurate design problems, adjoint-based shape optimization is a promising option. However, efficient sensitivity analysis should also be accompanied by a significant decrease in computational cost for the primal flow solution, as well. Reduced-order models, like those based on the harmonic balance concept, in combination with the calculation of gradients via adjoint methods, are proposed for the efficient solution of a certain class of aerodynamics optimization problems. The harmonic balance method is applicable if the flow is characterized by discrete finite dominant flow frequencies that do not need to be integer multiples of a fundamental harmonic. A fully-turbulent harmonic balance discrete adjoint formulation based on a duality-preserving approach is proposed. The method is implemented by leveraging algorithmic differentiation and is applied to two test cases: the constrained shape optimization of both a pitching airfoil and a turbine cascade. A key advantage of the current approach is the accurate computation of gradients as compared to second order finite differences without any approximation in the linearization of the turbulent viscosity. The shape optimization results show significant improvements for the selected time-dependent objective functions, demonstrating that design problems involving almost-periodic unsteady flows can be tackled with manageable computational effort.

Highlights

  • The proposed Harmonic Balance method (HB)-based adjoint method has been applied to two test cases: the fluid dynamic shape optimization of both a pitching airfoil and a turbine cascade

  • The framework enables shape optimization for quasi-periodically forced nonlinear fluid problems characterized by a set of frequencies that are not necessarily integer multiple of one fundamental harmonic

  • The results of the two test cases have clearly demonstrated that the method is capable of providing accurate gradients in the unsteady setting, as compared to sensitivities computed by second-order finite differences

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Summary

Introduction

The advancement of computational resources has enabled the application of CFD-based design methods to complex shapes, discretized on large domains, often in combination with high fidelity models [1,2]. In applications where the number of design variables is considerably greater than the number of objective functions, adjoint methods allow the computation of optimal solutions in the most cost-effective way, making them well suited for complex industrial applications [8,9,10]. Unsteady adjoint-based optimization methods can pave the way to the solution of multidisciplinary problems characterized by time-dependent phenomena such as those encountered in aeroelasticity or noise reduction [12], for example. Given the computational cost of accurately obtaining an unsteady solution and its adjoint, sufficiently accurate reduced order methods [13] must be used, if the objective is to solve design problems routinely. An airfoil pitching at a rate characterized by two frequencies that are not harmonically related is first considered, followed by a turbine cascade subject to unsteady inlet conditions

Time discretization
Harmonic balance operator
Time-domain harmonic balance
Governing equations of the adjoint solver
Results
NACA64A010 pitching airfoil
OptC1 configuration
Conclusions
Full Text
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