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patch to the topwing

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This commit is contained in:
Andy Killorin 2023-11-03 14:10:11 -05:00
parent 2f00aaec57
commit 7e9cd942fb
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GPG key ID: 8CB11B45B690DC2A
2 changed files with 11 additions and 5 deletions
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2
src/constants.rs
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@ -23,4 +23,4 @@ pub const ELEVATOR_CHORD: f32 = 5.0 *IN2MM;
pub const ELEVATOR_TAPER: f32 = 0.7; pub const ELEVATOR_TAPER: f32 = 0.7;
pub const ELEVATOR_STRUTS: usize = 4; pub const ELEVATOR_STRUTS: usize = 4;
pub const STOCK_HEIGHT: f32 = 25.0 *IN2MM; pub const STOCK_HEIGHT: f32 = 25.0 *IN2MM;
pub const STOCK_WIDTH: f32 = 36.0 *IN2MM; pub const STOCK_WIDTH: f32 = 37.0 *IN2MM;

14
src/main.rs
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@ -38,7 +38,13 @@ fn main() {
for port in [true,false] { for port in [true,false] {
let mut wing = wing(&wing_airfoil, STRUTS/2, WINGSPAN/2.0, CHORD, CHORD * WING_TAPER, SparType::Top); let mut wing = wing(&wing_airfoil, STRUTS/2, WINGSPAN/2.0, CHORD, CHORD * WING_TAPER, SparType::Top);
let top_spar = topwing_spar(&wing_airfoil, STRUTS/2, WINGSPAN/2.0, CHORD, CHORD * WING_TAPER); let top_spar = topwing_spar(&wing_airfoil, STRUTS/2, WINGSPAN/2.0, CHORD, CHORD * WING_TAPER);
register_part(scad!(Projection(false); top_spar));
let mut top_spar_neg = scad!(Difference; top_spar);
top_spar_neg.add_child(wing.clone());
wing.add_child(scad!(NamedColor("red".to_string()); top_spar_neg.clone()));
register_part(scad!(Projection(false); top_spar_neg));
wing = scad!(Translate(vec3(0.0, FUSELAGE_GAP,0.0)); wing); wing = scad!(Translate(vec3(0.0, FUSELAGE_GAP,0.0)); wing);
if port { if port {
wing = scad!(Mirror(vec3(0.0, 1.0, 0.0)); wing); wing = scad!(Mirror(vec3(0.0, 1.0, 0.0)); wing);
@ -64,7 +70,7 @@ fn main() {
// elevator // elevator
let mut elevator = scad!(Translate(vec3(LENGTH-ELEVATOR_CHORD, 0.0,0.0))); let mut elevator = scad!(Translate(vec3(LENGTH-ELEVATOR_CHORD, 0.0,0.0)));
for port in [true,false] { for port in [true,false] {
let mut wing = wing(&control_airfoil, ELEVATOR_STRUTS, ELEVATOR_HEIGHT, ELEVATOR_CHORD, ELEVATOR_CHORD * ELEVATOR_TAPER, SparType::Top); let mut wing = wing(&wing_airfoil, ELEVATOR_STRUTS, ELEVATOR_HEIGHT, ELEVATOR_CHORD, ELEVATOR_CHORD * ELEVATOR_TAPER, SparType::Top);
wing = scad!(Translate(vec3(0.0, FUSELAGE_GAP,0.0)); wing); wing = scad!(Translate(vec3(0.0, FUSELAGE_GAP,0.0)); wing);
if port { if port {
wing = scad!(Mirror(vec3(0.0, 1.0, 0.0)); wing); wing = scad!(Mirror(vec3(0.0, 1.0, 0.0)); wing);
@ -252,8 +258,8 @@ fn topwing_spar(aerofoil: &Airfoil, struts: usize, length: f32, chord: f32, tape
let mut last_t = scad!(Translate(vec3(0.0, -gap ,0.0))); let mut last_t = scad!(Translate(vec3(0.0, -gap ,0.0)));
last_t.add_child(scad!(LinearExtrude(extrude.clone()); last)); last_t.add_child(scad!(LinearExtrude(extrude.clone()); last));
hull.add_child(last_t); //hull.add_child(last_t);
hull.add_child(scad!(LinearExtrude(extrude); shape.clone())); //hull.add_child(scad!(LinearExtrude(extrude); shape.clone()));
transform.add_child(hull); transform.add_child(hull);
} }