[1] P. Batten, M. A. Leschziner, and U. C. Goldberg:
Average-state Jacobians and implicit methods for compressible viscous and turbulent flows. J. Comput. Phys. 137 (1997), 38–78.
MR 1481884
[2] D. M. Causon:
High resolution fnite volume schemes and computational aerodynamics. In: Nonlinear Hyperbolic Equations – Theory, Computation Methods and Applications (Notes on Numerical Fluid Mechanics volume 24, J. Ballmann and R. Jeltsch, eds.), Vieweg, Braunschweig 1989, pp. 63–74.
MR 0991352
[3]
Compendium of Unsteady Aerodynamic Measurements. AGARD Advisory Report No. 702, 1982.
[4] J. Donea: An arbitrary Lagrangian–Eulerian finite element method for transient fluid- structur interactions. Comput. Methods Appl. Mech. Engrg. 33 (1982), 689–723.
[5] M. Feistauer, J. Felcman, and I. Straškraba:
Mathematical and Computational Methods for Compressible Flow. (Numerical Mathematics and Scientific Computation.) Oxford University Press, Oxford 2003.
MR 2261900
[6] J. Fürst: Numerical Solution of Transonic Flow Using Modern Schemes of Finite volume Method and Finite Differences. Ph.D. Thesis (in Czech), ČVUT, Praha 2001.
[7] J. Fürst: A weighted least square scheme for compressible flows. Submitted to Flow, Turbulence and Combustion 2005.
[8] J. Fürst, M. Janda, and K. Kozel:
Finite volume solution of 2D and 3D Euler and Navier–Stokes equations. Math. Fluid Mechanics (J. Neustupa and P. Penel, eds.), Birkhäuser Verlag, Basel 2001.
MR 1865053
[9] J. Fürst and K. Kozel:
Application of second order TVD and ENO schemes in internal aerodynamics. J. Sci. Comput. 17 (2002), 1–4, 263–272.
MR 1910566
[10] J. Fürst and K. Kozel: Second and third order weighted ENO scheme on unstructured meshes. In: Proc. Finite Volumes for Complex Applications III (D. Herbin and D. Kröner, eds.), Hermes Penton Science, pp. 737–744.
[11] Kyu Hong Kim, Chongam Kim, and Oh-Hyun Rho:
Methods for the accurate computations of hypersonic flows. AUSMPW+ scheme. J. Comput. Physics 174 (2001), 38–80.
MR 1869671
[12] M. Lesoinne and C. Farhat: Geometric conservation laws for flow problems with moving boundaries and deformable meshes, and their impact on aeroelastic computations. Comput. Methods Appl. Mech. Engrg. 134 (1996), 71–90.
[13] V. Schmitt and F. Charpin: Pressure Distributions on the ONERA-M6-Wing at Transonic Mach Numbers. Experimental Data Base for Computer Program Assessment. Report of the Fluid Dynamics Panel Working Group 04, AGARD AR 138, 1979.
[14] H. C. Yee: A Class of High-Resolution Explicit and Implicit Shock-Capturing Methods. Technical Memorandum 101088, NASA, Moffett Field, California 1989.