Abstract
The current main chapter contains 14 contributions which cover all applications treated within the context of UNSI. Emphasis was placed on cross comparison of data in order to support potential scientists in their own work on validation/verification of all these test cases.
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References
Baldwin, B., and Lomax, H., Thin Layer Approximation and Algebraic Model for Separated Turbulent Flow, AIAA-78–257, 1978.
Eliasson, P., and Nordström, J., The Development of an Unsteady Solver for Moving Meshes, FFA TN 1995–39, 1995.
Jameson, A., Time Dependent Calculations using Multigrid, with Applications to Unsteady Flows past Airfoils and Wings, AIAA-91–1596, 1991.
Lacor, C., Zhu, Z.W., and Hirsch, C., A New Family of Limiters Within the Multigrid/Multiblock Navier-Stokes code Euranus, AIAA/DGLR 5th Int. Aerospace Planes and Hypersonics Conf., Munich. 1993.
McDevitt, J., Supercritical Flow about a Thick Circular-Arc Airfoil, NASA TM-78549, 1979.
Rizzi, A., Eliasson, P., Lindblad, I.,, Hirsch, C., Lacor, C., and Häuser, S., The Engineering of Multiblock/Multigrid Software for Navier-Stokes Flows on Structured Meshes, Computers & Fluids, 22, 1993, pp. 341–367.
Rumsey, C. L., Sanetrik, M. D., Biedron, R. T, Melson, N. D., and Parlette, E. B., Efficiency and Accuracy of Time-Accurate Turbulent Navier-Stokes Computations, AIAA-95–1835, 1995.
Tysell, L, and Hedman, S. G., Towards a general three-dimensional grid generation system, ICAS Paper 88–4. 7. 4. 1988.
Wallin, S., and Johansson A. V, An explicit algebraic Reynolds stress model of incompressible and compressible flows, J. Fluid Mech., 403, 2000, pp. 341–367.
Wilcox, D.C., Simulation of transition with a two-equation turbulence model, AIAA Journal 32, 1994, pp. 247–255.
Lee-Rauch, E., Batina, J. (1993): Wing Flutter Boundary Prediction Using Euler Aerodynamic Method. AIAA/ASME Adaptive Structures Forum, La Jolla, CA, Apr. 19–22, 1993
Gordiner, R., Melville, R. (2000): Transonic Flutter Simulations Using an Implicit Aeroelastic Solver. Journal of Aircraft Vol. 37, No. 5, September-October 2000.
Gupta, K. (1996): Development of a Finite Element Aeroelastic Analysis Capability. Journal of Aircraft Vol. 33, No. 5, September-October 1996.
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Barakos, G. et al. (2003). Application-oriented synthesis of work. In: Haase, W., Selmin, V., Winzell, B. (eds) Progress in Computational Flow-Structure Interaction. Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM), vol 81. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-45489-2_4
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DOI: https://doi.org/10.1007/978-3-540-45489-2_4
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