Computational methods and engineering applications of static/dynamic aeroelasticity based on CFD/CSD coupling solution

The CFD/CSD coupling method is turning into the main research direction for the static/dynamic aeroelastic analyses. If one wants to use the method for the complex engineering aeroelastic problems, he needs to investigate the relative aeroelastic algorithms, such as the numerical computational method of unsteady aerodynamic forces, equivalent low-dimensional structural finite element model and the solution method of structural dynamic equations, data transfer technique between fluid and structure, the moving grid method, etc. Besides, he also needs to improve the computational efficiency by such as massive parallel CFD algorithm, reduced-order model (ROM) of unsteady aerodynamic forces, etc. In this paper, based on the authors’ recent investigations, the research progresses in computational aeroelastic methods and their applications to engineering problem are summarized.

[1]  John T. Batina,et al.  Wing flutter computations using an aerodynamic model based on the Navier-Stokes equations , 1996 .

[2]  Aditi Chattopadhyay,et al.  A Volterra Kernel Reduced-Order Model Approach for Nonlinear Aeroelastic Analysis , 2005 .

[3]  P. Roe Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes , 1997 .

[4]  F. Menter Two-equation eddy-viscosity turbulence models for engineering applications , 1994 .

[5]  Juan J. Alonso,et al.  Fully-implicit time-marching aeroelastic solutions , 1994 .

[6]  H. Wendland,et al.  Working Title: Topics in Multivariate Approximation and Interpolation Computational Aspects of Radial Basis Function Approximation , 2022 .

[7]  S. Obayashi,et al.  Aileron Buzz Simulation Using an Implicit Multiblock Aeroelastic Solver , 2003 .

[8]  Ning Qin,et al.  Fast dynamic grid deformation based on Delaunay graph mapping , 2006 .

[9]  Andrew Arena,et al.  Acceleration CFD-based aeroelastic predictions using system identification , 1998 .

[10]  K. Nakahashi,et al.  Reordering of Hybrid Unstructured Grids for Lower-Upper Symmetric Gauss-Seidel Computations , 1998 .

[11]  Graham V. Candler,et al.  Data-parallel lower-upper relaxation method for the navier-stokes equations , 1996 .

[12]  Y. Zhu,et al.  Unsteady flow calculations with a multi-block moving mesh algorithm , 2000 .

[13]  V. Venkatakrishnan On the accuracy of limiters and convergence to steady state solutions , 1993 .

[14]  M. Liou A Sequel to AUSM , 1996 .

[15]  D. Ghate,et al.  Using Automatic Differentiation for Adjoint CFD Code Development , 2005 .

[16]  E C Yates,et al.  AGARD Standard Aeroelastic Configurations for Dynamic Response I - Wing 445.6 , 1988 .

[17]  J. Batina Unsteady Euler airfoil solutions using unstructured dynamic meshes , 1989 .

[18]  C. Farhat,et al.  Torsional springs for two-dimensional dynamic unstructured fluid meshes , 1998 .

[19]  Earl H. Dowell,et al.  System Identii Cation and Proper Orthogonal Decomposition Method Applied to Unsteady Aerodynamics , 2022 .

[20]  F. Menter Improved two-equation k-omega turbulence models for aerodynamic flows , 1992 .

[21]  A. Jameson,et al.  Lower-upper Symmetric-Gauss-Seidel method for the Euler and Navier-Stokes equations , 1988 .

[22]  Guru P. Guruswamy,et al.  VORTICAL FLOW COMPUTATIONS ON SWEPT FLEXIBLE WINGS USING NAVIER-STOKES EQUATIONS , 1989 .

[23]  Vipin Kumar,et al.  Multilevel k-way hypergraph partitioning , 1999, DAC '99.

[24]  Raymond E. Gordnier,et al.  Transonic flutter simulations using an implicit aeroelastic solver , 2000 .

[25]  S. Obayashi,et al.  Convergence acceleration of an aeroelastic Navier-Stokes solver , 1994 .

[26]  F. Menter ZONAL TWO EQUATION k-w TURBULENCE MODELS FOR AERODYNAMIC FLOWS , 1993 .

[27]  P. Lax,et al.  On Upstream Differencing and Godunov-Type Schemes for Hyperbolic Conservation Laws , 1983 .

[28]  Clarence O. E. Burg,et al.  A Robust Unstructured Grid Movement Strategy using Three-Dimensional Torsional Springs , 2004 .