Development of a Steady Potential Solver for Use with Linearized Unsteady Aerodynamic Analyses

Author:

Hoyniak Daniel,Verdon Joseph M.

Publisher

Springer New York

Reference15 articles.

1. Atassi, H., and Akai, Ti., 1980, “Aerodynamic and aeroelastic Characteristics of Oscillating Loaded Cascades at Low Mach Number. I Pressure Distribution, Forces and Moments,” Transactions of American Society of Mechanical Engineering Journal of Engineering for Power, Vol 102,No. 2, pp. 344–351.

2. Bailey, H.E. and Beam, R.M., 1991, “Newton’s Method Applied to Finite-Difference Approximations for the Steady-State Compressible Navier-Stokes Equations”, Journal of Computational Physics, Vol 93., pp 108–127.

3. Bender, E.E., and Khosla, P.K., 1988, “Application of Sparse Matrix Solvers and Newton’s Method to Fluid Flow Problems”, AIAA paper number 88–3700CP.

4. Bôlcs, A., and Fransson, T.H., 1986, “Aeroelasticity in Turbomachines - Comparison of Theoretical and Experimential Cascade Results”, Communication du Laboratorie de Thermique Appliquèe et de Turbomachines, No. 13, Lausanne, EPFL.

5. Caruthers, J.E., and Dalton, W.N., 1991, “Unsteady Aerodynamic Response of a Cascade to Nonuniform Inflow,” ASME Paper 91-GT-174, Presented at the International Gas Turbine and Aeroengine Congress and Exposition, Orlando, Florida, June 3–6, 1991.

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