28.01.2013 Views

Zienkiewicz O.C., Taylor R.L. Vol. 3. The finite - tiera.ru

Zienkiewicz O.C., Taylor R.L. Vol. 3. The finite - tiera.ru

Zienkiewicz O.C., Taylor R.L. Vol. 3. The finite - tiera.ru

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

214 Compressible high-speed gas ¯ow<br />

2<strong>3.</strong> O. Hassan, K. Morgan and J. Peraire. An implicit±explicit scheme for compressible viscous<br />

high speed ¯ows. Comp. Meth. Appl. Mech. Eng., 76, 245±58, 1989.<br />

24. N.P. Weatherill, E.A. Turner-Smith, J. Jones, K. Morgan and O. Hassan. An integrated<br />

software environment for multi-disciplinary computational engineering. Engng. Comp.,<br />

16, 913±33, 1999.<br />

25. P.M.R. Lyra and K. Morgan. A review and comparative study of upwind biased schemes<br />

for compressible ¯ow computation. Part I: 1-D ®rst-order schemes. Arch. Comp. Meth.<br />

Engng., 7, 19±55, 2000.<br />

26. K. Morgan and J. Peraire. Unst<strong>ru</strong>ctured grid ®nite element methods for ¯uid mechanics.<br />

Rep. Prog. Phys., 61, 569±638, 1998.<br />

27. R. Ayers, O. Hassan, K. Morgan and N.P. Weatherill. <strong>The</strong> role of computational ¯uid<br />

dynamics in the design of the Th<strong>ru</strong>st supersonic car. Design Optim. Int. J. Prod. & Proc.<br />

Improvement, 1, 79±99, 1999.<br />

28. K. Morgan, O. Hassan and N.P. Weatherill. Why didn't the supersonic car ¯y? Mathematics<br />

Today, Bulletin of the Institute of Mathematics and its Applications, 35, 110±14, Aug. 1999.<br />

29. O. Hassan, L.B. Bayne, K. Morgan and N.P. Weatherill. An adaptive unst<strong>ru</strong>ctured mesh<br />

method for transient ¯ows involving moving boundaries. ECCOMAS '98, Wiley, New York.<br />

30. O. Hassan, E.J. Probert, N.P. Weatherill, M.J. Marchant and K. Morgan. <strong>The</strong> numerical<br />

simulation of viscous transonic ¯ow using unst<strong>ru</strong>ctured grids, AIAA-94-2346, June 20±23,<br />

Colorado Springs, USA.<br />

31. O. Hassan, E.J. Probert, K. Morgan and J. Peraire. Mesh generation and adaptivity for the<br />

solution of compressible viscous high speed ¯ows. Int. J. Num. Meth. Eng., 38, 1123±48, 1995.<br />

32. O. Hassan, K. Morgan, E.J. Probert and J. Peraire. Unst<strong>ru</strong>ctured tetrahedral mesh generation<br />

for three dimensional viscous ¯ows. Int. J. Num. Meth. Eng., 39, 549±67, 1996.<br />

3<strong>3.</strong> O. Hassan, E.J. Probert and K. Morgan. Unst<strong>ru</strong>ctured mesh procedures for the simulation<br />

of three dimensional transient compressible inviscid ¯ows with moving boundary components.<br />

Int. J. Num. Meth. Fluids, 27, 41±55, 1998.<br />

34. M.T. Manzari, O. Hassan, K. Morgan and N.P. Weatherill. Turbulent ¯ow computations<br />

on 3D unst<strong>ru</strong>ctured grids. Finite Elements in Analysis and Design, 30, 353±63, 1998.<br />

35. E.J. Probert, O. Hassan and K. Morgan. An adaptive ®nite element method for<br />

transient compressible ¯ows with moving boundaries. Int. J. Num. Meth. Eng., 32, 751±<br />

65, 1991.<br />

36. K. Morgan, N.P. Weatherill, O. Hassan, P.J. Brookes, R. Said and J. Jones. A parallel<br />

framework for multidisciplinary aerospace engineering simulations using unst<strong>ru</strong>ctured<br />

meshes. Int. J. Num. Meth. Fluids, 31, 159±73, 1999.<br />

37. K. Morgan, P.J. Brookes, O. Hassan and N.P. Weatherill. Parallel processing for the<br />

simulation of problems involving scattering of electromagnetic waves. Comp. Meth.<br />

Appl. Mech. Eng., 152, 157±74, 1998.<br />

38. R. Said, N.P. Weatherill, K. Morgan and N.A. Verhoeven. Distributed parallel Delaunay<br />

mesh generation. Comp. Meth. Appl. Mech. Eng., 177, 109±25, 1999.<br />

39. C. Hirsch. Numerical Computation of Internal and External Flows. <strong>Vol</strong>. I, Wiley, Chichester,<br />

1988.<br />

40. L. Demkowicz, J.T. Oden and W. Rachowicz. A new ®nite element method for solving<br />

compressible Navier±Stokes equations based on an operator splitting method and h-p<br />

adaptivity. Comp. Meth. Appl. Mech. Eng., 84, 275±326, 1990.<br />

41. J. Vadyak, J.D. Ho€man and A.R. Bishop. Flow computations in inlets at incidence using<br />

a shock ®tting Bicharacteristic method. AIAA Journal, 18, 1495±502, 1980.<br />

42. K.W. Morton and M.F. Paisley. A ®nite volume scheme with shock ®tting for steady Euler<br />

equations. J. Comp. Phys., 80, 168±203, 1989.<br />

4<strong>3.</strong> J. von Neumann and R.D. Richtmyer. A method for the numerical calculations of hydrodynamical<br />

shocks. J. Math. Phys., 21, 232±7, 1950.

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!