By M. O. Bristeau, R. Glowinski, J. Periaux (auth.), Marie Odile Bristeau, Roland Glowinski, Jacques Periaux, Henri Viviand (eds.)
With the arrival of large desktops over the last ten years, the numerical simulation of viscous fluid flows modeled through the Navier-Stokes equations is changing into a most respected device in plane and Engine layout. actually, compressible Navier-Stokes solvers are inclined to represent the elemental instruments for plenty of business functions occuring within the simulation of very advanced turbulent and combustion phenomena. In Aerospace Engineering, as an exemple, their mathematical modelization calls for trustworthy and strong equipment for fixing very stiff non linear partial differential equations. For the above purposes, it used to be transparent workshop in this subject will be of curiosity for the CFD neighborhood for you to evaluate accuracy and potency of Navier-Stokes solvers on chosen exterior and inner move difficulties utilizing diverse numerical ways. The workshop used to be hung on 4-6 December 1985 at great, France and arranged via INRIA with the sponsorship of the GAMM Committee on Numerical equipment in Fluid Mechanics.
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C) Reo 30 Y at x -10. a) Reo = 100, b) Reo = 400, MACH 0011 --1 Reo = 1600 0010 -----2 -----3 0008 0007 0006 0005 0004 0003 0002 0001 00 00 100 Fig. 9 200 300 400 500 600 700 Y Mach number profiles at x = -10. P IPO 009970 009965 009960 009955 -1 009950 ------2 ----3 ---5 I 00 Fig. 10 I I 200 I I I I 300 I I I I 400 I I I I I 500 Pressure profiles at x = -10. - Oe9998 -''-1'''''1""1""1'-""1"-''-'1''-''-'1-''-'1''-'1''-'1''-'1 1 cO 2eO 3eO 4eO 5eO 6eO 7 cO Oe y Fig. 11 U/AO S1 profiles at x = -10 (S1 = (p/po)·(Po/P)Y).
A numerical method for threedimensional viscous flow : application to the hypersonic leading edge", J. Comput. Phys. , 339-364, 1972. B. L. , ~, 1421-1430, 1980. P. "A computational procedure for supersonic flows governed by the parabolic Navier-Stokes equations", J. Comput. , ~, 356-380, 1980. S. S. "Computation of hypersonic viscous flow around three-dimensional bodies at high angles of attack", AIAA paper 81-1261, 1981. S. M. "Calculation of viscous supersonic flow over finned bodies", AlAA paper 83-1667, 1983.
120 x CF 0010 0009 0008 0007 0006 0005 0004 0003 0002 0001 1 1 '-1 1 1 1 1 1 1 1 1 1 1 1 ------2 -I ----3 a) -I 1 1 1 1 1 1 1 1 1 - 1 - 1 1 \ \ 00 x. -0001 CF 00050 -~,20 00045 - 00040 - -80 40 -40 120 -1 ------2 ----3 00035 00030 80 ---4 - ---5 00025 00020 - 00015 - 00010 - 00005 - b) 00 -00005 -, "" , ' , -4('1 Or: ·-120-80 Fig. e~ = 400 and 1600. I i I I ' i I 4, distributions. I ' :-L- -,-,-; 121 a) Reo = lOU, 25 CH OD010 --1 OD009 ------2 OD008 ----3 OD007 OD006 Reo = 100 a) OD005 OD004 OD003 OD002 OD001 OD -12D -8D -4D OD 4D 8D 12D X CH OD0050 --I OD0045 ---- -2 OD0040 ----3 OD0035 ---4 OD0030 b) OD0025 OD0020 ODOO15 OD0010 000005 00 -120 Fig.