Read time: 4.6 minutes (457 words)
Data CatalogΒΆ
Name |
Value |
File |
---|---|---|
a |
||
stub_length |
fuselage/rear_hook/rear_hook_data.scad |
|
tip_dihedral |
wing/wing_data.scad |
|
b |
||
ms_height - wire_diameter |
fuselage/rear_hook/rear_hook_data.scad |
|
(max_projected_wing_span - center_span)/2 |
wing/wing_data.scad |
|
bend_radius |
||
1.5*wire_diameter |
fuselage/rear_hook/rear_hook_data.scad |
|
c |
||
2.5 |
prop/prop_data.scad |
|
hook_side |
fuselage/rear_hook/rear_hook_data.scad |
|
center_span |
||
6 |
stab/stab_data.scad |
|
12 |
wing/wing_data.scad |
|
density |
||
501.12 |
fuselage/rear_hook/rear_hook_data.scad |
|
168.77 |
fuselage/thrust_bearing/thrust_bearing_data.scad |
|
6 |
fuselage/tail_boom/tail_boom_data.scad |
|
f |
||
2 |
prop/prop_data.scad |
|
fin_chord |
||
4 |
fuselage/fin/fin_data.scad |
|
fin_color |
||
WOOD_Balsa |
fuselage/fin/fin_data.scad |
|
fin_le_length |
||
fin_span - fin_radius - spar_size |
fuselage/fin/fin_data.scad |
|
fin_radius |
||
1.5 |
fuselage/fin/fin_data.scad |
|
fin_span |
||
2 |
fuselage/fin/fin_data.scad |
|
fin_te_length |
||
fin_span -2*spar_size |
fuselage/fin/fin_data.scad |
|
fp_offset |
||
wing_offset - post_diameter/2 - tube_thickness |
fuselage/fuselage_data.scad |
|
fuse_offset |
||
thb_length - thb_top_length - 3 * tube_thickness |
fuselage/fuselage_data.scad |
|
hook_offset |
||
thb_height |
fuselage/rear_hook/rear_hook_data.scad |
|
hook_side |
||
(hook_offset - 2*bend_radius*ka)/ka |
fuselage/rear_hook/rear_hook_data.scad |
|
ka |
||
sin(45) |
fuselage/rear_hook/rear_hook_data.scad |
|
motor_stick_rear_height |
||
0.1875 |
fuselage/motor_stick/motor_stick_data.scad |
|
motor_stick_thickness |
||
1/8 |
math_magik_lpp_data.scad |
|
ms_height |
||
motor_stick_rear_height |
fuselage/rear_hook/rear_hook_data.scad |
|
ms_length |
||
10 |
fuselage/motor_stick/motor_stick_data.scad |
|
ms_points |
||
fuselage/motor_stick/motor_stick_data.scad |
||
ms_thickness |
||
1/8 |
fuselage/motor_stick/motor_stick_data.scad |
|
num_center_ribs |
||
3 |
stab/stab_data.scad |
|
5 |
wing/wing_data.scad |
|
p1 |
||
[-bend_radius,0,b] |
fuselage/rear_hook/rear_hook_data.scad |
|
p2 |
||
[-bend_radius,0,0] |
fuselage/rear_hook/rear_hook_data.scad |
|
p3 |
||
p2 + [bend_radius*ka,0,-bend_radius*ka] |
fuselage/rear_hook/rear_hook_data.scad |
|
p4 |
||
p3 + [-hook_side*ka, 0,-hook_side*ka] + [bend_radius*ka,0,-bend_radius*ka] |
fuselage/rear_hook/rear_hook_data.scad |
|
p5 |
||
p4 + [-bend_radius*ka,0,-bend_radius*ka] |
fuselage/rear_hook/rear_hook_data.scad |
|
post_size |
||
1/16 |
math_magik_lpp_data.scad |
|
prop_blade_color |
||
WOOD_Balsa |
prop/prop_data.scad |
|
prop_blade_offset |
||
0.5 |
prop/prop_data.scad |
|
prop_blade_thickness |
||
1/64 |
prop/prop_data.scad |
|
prop_form_angle |
||
14 |
prop/prop_data.scad |
|
prop_form_height |
||
prop_radius + 2 |
prop/prop_data.scad |
|
prop_form_radius |
||
2.5 |
prop/prop_data.scad |
|
prop_forward_x |
||
-1.3287 |
prop/prop_data.scad |
|
prop_max_chord |
||
1.85 |
prop/prop_data.scad |
|
prop_pitch_angle |
||
40 |
prop/prop_data.scad |
|
prop_radius |
||
max_prop_diameter/2 |
prop/prop_data.scad |
|
prop_spar_color |
||
WOOD_Balsa |
prop/prop_data.scad |
|
prop_spar_inner_radius |
||
1/32 |
prop/prop_data.scad |
|
prop_spar_length |
||
4 |
prop/prop_data.scad |
|
prop_spar_outer_radius |
||
1/64 |
prop/prop_data.scad |
|
prop_x_offset |
||
-1/4 - 1/32 |
math_magik_lpp_data.scad |
|
1/16 |
fuselage/fuselage_data.scad |
|
prop_x_width |
||
1.3287 |
math_magik_lpp_data.scad |
|
prop_z_offset |
||
-3/16 |
math_magik_lpp_data.scad |
|
thb_height |
fuselage/fuselage_data.scad |
|
r |
||
wire_diameter/2 |
fuselage/rear_hook/rear_hook_data.scad |
|
rear_hook_color |
||
METAL_Steel |
fuselage/rear_hook/rear_hook_data.scad |
|
rib_camber |
||
2 |
stab/stab_data.scad |
|
4 |
wing/wing_data.scad |
|
rib_chord |
||
max_stab_chord - 2 * spar_size |
stab/stab_data.scad |
|
max_wing_chord - 2 * spar_size |
wing/wing_data.scad |
|
rp_offset |
||
wing_offset + max_wing_chord + post_diameter/2 + tube_thickness |
fuselage/fuselage_data.scad |
|
rubber_motor_length |
||
10 |
rubber_motor/rubber_motor_data.scad |
|
rubber_motor_radius |
||
1/8 |
rubber_motor/rubber_motor_data.scad |
|
s |
||
prop_radius - 1 |
prop/prop_data.scad |
|
s1 |
||
1 |
prop/prop_data.scad |
|
s2 |
||
s - s1 |
prop/prop_data.scad |
|
s3 |
||
1 |
prop/prop_data.scad |
|
s4 |
||
1 |
prop/prop_data.scad |
|
sfp_offset |
||
srp_offset - max_stab_chord - post_diameter - tube_thickness-1/64 |
fuselage/fuselage_data.scad |
|
spar_size |
||
1/16 |
stab/stab_data.scad |
|
1/32 |
fuselage/fin/fin_data.scad |
|
1/16 |
wing/wing_data.scad |
|
srp_offset |
||
tail_boom_rear_x - post_diameter - tube_thickness-1/16 |
fuselage/fuselage_data.scad |
|
stab_center_span |
||
6 |
math_magik_lpp_data.scad |
|
stab_elevation |
||
0.5 |
math_magik_lpp_data.scad |
|
stab_post_color |
||
WOOD_Balsa |
fuselage/stab_post/stab_post_data.scad |
|
stab_post_height |
||
0.5 + tube_height |
fuselage/stab_post/stab_post_data.scad |
|
stab_rib_camber |
||
2 |
math_magik_lpp_data.scad |
|
stab_tip_radius |
||
1.5 |
math_magik_lpp_data.scad |
|
stab_x_offset |
||
max_overall_length - prop_x_width - max_stab_chord |
math_magik_lpp_data.scad |
|
stub_length |
||
1/8 |
fuselage/rear_hook/rear_hook_data.scad |
|
tail_boom_angle |
||
atan2(tb_front_height - tb_rear_height,tail_boom_length) |
fuselage/fuselage_data.scad |
|
atan2(tb_front_height - tb_rear_height,tail_boom_length) |
fuselage/tail_boom/tail_boom_data.scad |
|
tail_boom_length |
||
max_overall_length -ms_length + prop_forward_x + tail_boom_overlap |
fuselage/fuselage_data.scad |
|
tail_boom_overlap |
||
1/8 |
fuselage/fuselage_data.scad |
|
tail_boom_rear_x |
||
max_overall_length + prop_x_offset |
fuselage/fuselage_data.scad |
|
tb_color |
||
WOOD_Balsa |
fuselage/fuselage_data.scad |
|
WOOD_Balsa |
fuselage/tail_boom/tail_boom_data.scad |
|
tb_front_height |
||
3/16 |
fuselage/fuselage_data.scad |
|
3/16 |
fuselage/tail_boom/tail_boom_data.scad |
|
tb_rear_height |
||
1/16 |
fuselage/fuselage_data.scad |
|
1/16 |
fuselage/tail_boom/tail_boom_data.scad |
|
tb_thickness |
||
3/32 |
fuselage/fuselage_data.scad |
|
3/32 |
fuselage/tail_boom/tail_boom_data.scad |
|
thb_front_height |
||
thb_height/3 |
fuselage/thrust_bearing/thrust_bearing_data.scad |
|
thb_height |
||
3/16 |
fuselage/thrust_bearing/thrust_bearing_data.scad |
|
thb_length |
||
1/2 |
fuselage/thrust_bearing/thrust_bearing_data.scad |
|
thb_thickness |
||
1/32 |
fuselage/thrust_bearing/thrust_bearing_data.scad |
|
thb_top_length |
||
3/16 |
fuselage/thrust_bearing/thrust_bearing_data.scad |
|
thb_width |
||
1/16 |
fuselage/thrust_bearing/thrust_bearing_data.scad |
|
thb_wire_size |
||
0.025 |
fuselage/thrust_bearing/thrust_bearing_data.scad |
|
thrust_bearing_color |
||
METAL_Aluminium |
fuselage/thrust_bearing/thrust_bearing_data.scad |
|
thrust_bearing_x_offset |
||
-1/4 |
math_magik_lpp_data.scad |
|
tip_dihedral |
||
1.75 |
wing/wing_data.scad |
|
tip_dihedral_angle |
||
atan2(a,b) |
wing/wing_data.scad |
|
tip_le_span |
||
tip_span - tip_radius |
stab/stab_data.scad |
|
tip_span - tip_radius |
wing/wing_data.scad |
|
tip_radius |
||
1.5 |
stab/stab_data.scad |
|
2 |
wing/wing_data.scad |
|
tip_rib_chord |
||
max_stab_chord - tip_radius - spar_size |
stab/stab_data.scad |
|
max_wing_chord - tip_radius - spar_size |
wing/wing_data.scad |
|
tip_span |
||
(max_stab_span - center_span)/2 |
stab/stab_data.scad |
|
sqrt(a*a + b*b) |
wing/wing_data.scad |
|
wing_center_span |
||
12 |
math_magik_lpp_data.scad |
|
wing_elevation |
||
3 |
math_magik_lpp_data.scad |
|
3 |
fuselage/fuselage_data.scad |
|
wing_offset |
||
1.625 |
fuselage/fuselage_data.scad |
|
wing_post_color |
||
WOOD_Balsa |
fuselage/wing_post/wing_post_data.scad |
|
wing_post_height |
||
wing_elevation + tube_height |
fuselage/wing_post/wing_post_data.scad |
|
wing_rib_camber |
||
4 |
math_magik_lpp_data.scad |
|
wing_spar_size |
||
1/16 |
math_magik_lpp_data.scad |
|
wing_tip_radius |
||
2 |
math_magik_lpp_data.scad |
|
wing_x_offset |
||
1.625 |
math_magik_lpp_data.scad |
|
wire_diameter |
||
0.025 |
fuselage/rear_hook/rear_hook_data.scad |