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################ GEOMETRY INPUT PARAMETERS ################
#
# Input file names:
set base_geometry_file		wbt_base.tin
#
# Output file names:
set geometry_file		wbt.tin
#
# ICEM geometric tolerances
set geo_tol			1.0E-7
#
# Farfield distance:
set farfield_dist		1000
set farfield_spread_angle	3.0
#
# Off-surface block size
set fuse_offset_dist		2.00
set fuse_flare_angle		45.00
set wing_chord_offset		1.00
set wing_normal_offset		2.00
set wing_tip_offset		5.00
set tail_chord_offset		2.00
set tail_normal_offset		2.00
set tail_tip_offset		8.00
#
# The 4 fuselage section curves (as frac of fuse length)
set fuse_sections	 { NOSE 0.1 0.2 LE HC TE 0.80 0.98 TAIL }
#
# Tail spanwise split fraction
set split_tail                  False
set tail_span_split             0.5
#

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