Simple Input File for Steady-State Viscous Flow

#Case title: This is a sample input file
Mach	alpha	beta	ReUe,mil	Tinf,dR	itwall	Tw/Tinf	ipwall
0.84	3.06	0.0	11.7	460.0	0	-1.0	0
sref	cref	bref	xmc	ymc	zmc
0.5255	0.667	1.0	0.0	0.0	0.0
ioverset	impl	cfl1	iramp	cfl2	cflmin	GS_tol	crelax
0	1	-20.0	50	150.0	5.0	0.0	1.0
itimeacc	delta_t	ntstep	res_step	imvgrd	isolavg	nbgnavg
0	0.3	500	-3.0	0	0	1500
irest	mstage	iresmth	dqmax	p_break	pmin	limiter
0	3	1	0.5	0.05	0.001	0.
nupdate	nwrest	nwflo	nwflobgn	ipltqn	idiagnos	nodeypl
1	500	-500	1500	2	0	0
iorder	lapl-avg	high-bc	ifds	ivisc	itrip	EV_lim
0	1	1	1	2	0	0.0
ncyc	nengines	nsinkbc	nrotor	compF&M	p_bc1002	cldes
1000	0	0	0	0	0.	0.

This is a typical USM3D input file for a standard computation of a transonic aircraft with no engines.

The RED denotes the primary parameters that will require attention from the user. The remaining parameters can generally remain unchanged.

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NASA Official Responsible For Content: Dr. Neal T. Frink
Site Curator: Dr. Neal T. Frink
Last Updated: August 8, 2003

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