Input File for Inlet Plane with Prescribed Mass 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	-150.0	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
50	75	100	1500	2	0	0
iorder	lapl-avg	high-bc	ifds	ivisc	itrip	EV_lim
2	1	1	1	3	0	0.0
ncyc	nengines	nsinkbc	nrotor	compF&M	p_bc1002	cldes
10	0	1	0	0	0.	0.
sinkid	outer_R	cen_X	cen_Y	cen_Z	massflx	omega
111	1.0	0.0	0.0	0.0	3.0	-0.5

RED denotes the primary parameters that will require attention from the user. GREEN denotes the parameters that will require attention from the user for this option. 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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