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Convergence Acceleration Of A Navier Stokes Solver For Efficient Static Aeroelastic Computations by S. Obayashi

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1NASA Technical Reports Server (NTRS) 19970009493: Convergence Acceleration Of A Navier-Stokes Solver For Efficient Static Aeroelastic Computations

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New capabilities have been developed for a Navier-Stokes solver to perform steady-state simulations more efficiently. The flow solver for solving the Navier-Stokes equations is based on a combination of the lower-upper factored symmetric Gauss-Seidel implicit method and the modified Harten-Lax-van Leer-Einfeldt upwind scheme. A numerically stable and efficient pseudo-time-marching method is also developed for computing steady flows over flexible wings. Results are demonstrated for transonic flows over rigid and flexible wings.

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  • Title: ➤  NASA Technical Reports Server (NTRS) 19970009493: Convergence Acceleration Of A Navier-Stokes Solver For Efficient Static Aeroelastic Computations
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  • Language: English

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