Optimum Shape Design for Unsteady Three-Dimensional Viscous Flows Using a Nonlinear Frequency-Domain Method

Thispaperpresentsanadjointmethodfortheoptimumshapedesignofunsteadythree-dimensionalviscous flows. The goal is to develop a set of discrete unsteady adjoint equations and the corresponding boundary condition for the nonlinear frequency-domain method. First, this paper presents the complete formulation of the time-dependent optimal design problem. Second, we present the nonlinear frequency-domain adjoint equations for threedimensional viscous transonic flows. Third, we present results that demonstrate the application of the theory to a three-dimensional wing.

[1]  Arthur David Snider,et al.  An Improved Estimate of the Accuracy of Trigonometric Interpolation , 1972 .

[2]  A. Jameson,et al.  Numerical solution of the Euler equations by finite volume methods using Runge Kutta time stepping schemes , 1981 .

[3]  A Jameson,et al.  Computational Aerodynamics for Aircraft Design , 1989, Science.

[4]  A. Jameson Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings , 1991 .

[5]  A. Jameson Optimum aerodynamic design using CFD and control theory , 1995 .

[6]  Juan J. Alonso,et al.  Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on distributed memory parallel computers , 1996 .

[7]  A. Jameson,et al.  Aerodynamic Shape Optimization of Complex Aircraft Configurations via an Adjoint Formulation , 1996 .

[8]  J. Adamczyk Model equation for simulating flows in multistage turbomachinery , 1996 .

[9]  Juan J. Alonso,et al.  Aerodynamic Shape Optimization of Supersonic Aircraft Configurations via an Adjoint Formulation on Parallel Computers , 1996 .

[10]  J. Alonso,et al.  Acceleration of Convergence to a Periodic Steady State in Turbomachinery Flows , 2001 .

[11]  Michael B. Giles,et al.  The harmonic adjoint approach to unsteady turbomachinery design , 2002 .

[12]  Jeffrey P. Thomas,et al.  Computation of Unsteady Nonlinear Flows in Cascades Using a Harmonic Balance Technique , 2002 .

[13]  Juan J. Alonso,et al.  Application of a Non-Linear Frequency Domain Solver to the Euler and Navier-Stokes Equations , 2002 .

[14]  Juan J. Alonso,et al.  SONIC BOOM REDUCTION USING AN ADJOINT METHOD FOR WING-BODY CONFIGURATIONS IN SUPERSONIC FLOW , 2002 .

[15]  Antony Jameson,et al.  OPTIMAL CONTROL OF UNSTEADY FLOWS USING A TIME ACCURATE METHOD , 2002 .

[16]  Earl H. Dowell,et al.  A Discrete Adjoint Approach for Modeling Unsteady Aerodynamic Design Sensitivities , 2003 .

[17]  S. Nadarajah,et al.  The discrete adjoint approach to aerodynamic shape optimization , 2003 .

[18]  Antony Jameson,et al.  OPTIMUM SHAPE DESIGN FOR UNSTEADY FLOWS USING TIME ACCURATE AND NON-LINEAR FREQUENCY DOMAIN METHODS , 2003 .

[19]  M. McMullen,et al.  The application of non-linear frequency domain methods to the Euler and Navier-Stokes equations , 2003 .

[20]  Antony Jameson,et al.  NON-LINEAR FREQUENCY DOMAIN BASED OPTIMUM SHAPE DESIGN FOR UNSTEADY THREE-DIMENSIONAL FLOWS , 2006 .