added WingConfig struct

src/constants.rs

@@ -1,3 +1,5 @@
+use crate::WingConfig;
+
 /// Constants
 /// the native unit is mm
 
@@ -8,6 +10,12 @@ pub const WINGSPAN: f32 = 45.0 * IN2MM;
 pub const LENGTH: f32 = 30.0 * IN2MM;
 /// strut count in the main wing
 pub const STRUTS: usize = 12;
+pub const WING: WingConfig = WingConfig {
+    length: WINGSPAN / 2.0,
+    chord: CHORD,
+    taper: WING_TAPER,
+    struts: STRUTS / 2,
+};
 pub const CARDBOARD_WIDTH: f32 = 3.5;
 /// length of each side of the triangular spar
 pub const SPAR_SIDE_WIDTH: f32 = 0.75 * IN2MM;
@@ -18,9 +26,21 @@ pub const RUDDER_HEIGHT: f32 = 5.0 * IN2MM;
 pub const RUDDER_CHORD: f32 = 3.0 * IN2MM;
 pub const RUDDER_TAPER: f32 = 0.7;
 pub const RUDDER_STRUTS: usize = 3;
+pub const RUDDER: WingConfig = WingConfig {
+    length: RUDDER_HEIGHT,
+    chord: RUDDER_CHORD,
+    taper: RUDDER_TAPER,
+    struts: RUDDER_STRUTS,
+};
 pub const ELEVATOR_HEIGHT: f32 = 8.0 * IN2MM;
 pub const ELEVATOR_CHORD: f32 = 5.0 * IN2MM;
 pub const ELEVATOR_TAPER: f32 = 0.7;
 pub const ELEVATOR_STRUTS: usize = 4;
+pub const ELEVATOR: WingConfig = WingConfig {
+    length: ELEVATOR_HEIGHT,
+    chord: ELEVATOR_CHORD,
+    taper: ELEVATOR_TAPER,
+    struts: ELEVATOR_STRUTS,
+};
 pub const STOCK_HEIGHT: f32 = 25.0 * IN2MM;
 pub const STOCK_WIDTH: f32 = 37.0 * IN2MM;

src/main.rs

@@ -36,7 +36,7 @@ fn main() {
     // symetric airfoil, used in the control surfaces
     let control_airfoil: SeligFile = SeligFile::parse(include_str!("../edgevertical.dat"));
 
-    let wing_transform = mirrored_wing(&wing_airfoil);
+    let wing_transform = mirrored_wing(&wing_airfoil, &WING);
 
     // spars
 
@@ -48,10 +48,7 @@ fn main() {
     let mut rudder = scad!(Rotate(90.0, vec3(1.0, 0.0, 0.0)));
     rudder.add_child(wing(
         &control_airfoil,
-        RUDDER_STRUTS,
-        RUDDER_HEIGHT,
-        RUDDER_CHORD,
-        RUDDER_CHORD * RUDDER_TAPER,
+        &RUDDER,
         SparType::Center,
     ));
     rudder.add_child(spar(RUDDER_HEIGHT, false));
@@ -64,10 +61,7 @@ fn main() {
     for port in [true, false] {
         let mut wing = wing(
             &wing_airfoil,
-            ELEVATOR_STRUTS,
-            ELEVATOR_HEIGHT,
-            ELEVATOR_CHORD,
-            ELEVATOR_CHORD * ELEVATOR_TAPER,
+            &ELEVATOR,
             SparType::Top,
         );
         let top_spar = topwing_spar(
@@ -135,7 +129,7 @@ impl Construct {
     }
 }
 
-fn mirrored_wing(wing_airfoil: &SeligFile) -> Construct {
+fn mirrored_wing(wing_airfoil: &SeligFile, wing_config: &WingConfig) -> Construct {
     let mut parts = Vec::new();
     let mut wing_transform = scad!(Translate(vec3(0.0, 0.0, 0.0)));
     // struts
@@ -143,10 +137,7 @@ fn mirrored_wing(wing_airfoil: &SeligFile) -> Construct {
     for port in [true, false] {
         let mut wing = wing(
             wing_airfoil,
-            STRUTS / 2,
-            WINGSPAN / 2.0,
-            CHORD,
-            CHORD * WING_TAPER,
+            &wing_config,
             SparType::Top,
         );
         let top_spar = topwing_spar(
@@ -189,9 +180,10 @@ enum SparType {
 }
 
 /// returns a extruded airfoil with the given dimensions
-fn strut(airfoil: &SeligFile, chord: f32, width: f32, spar: &SparType) -> ScadObject {
+fn strut(airfoil: &SeligFile, chord: f32, width: f32, spar: &SparType) -> Construct {
     let aerofoil = scad::PolygonParameters::new(airfoil.get_points().to_vec());
     let shape = scad!(Polygon(aerofoil));
+    let mut parts = Vec::new();
 
     let strut_hole = {
         match spar {
@@ -205,7 +197,29 @@ fn strut(airfoil: &SeligFile, chord: f32, width: f32, spar: &SparType) -> ScadOb
         }
     };
 
-    extrude_strut(shape, strut_hole, width, chord, true)
+    let shape = shape;
+    let chord = chord;
+    let mut strut_shape = scad!(Difference);
+    strut_shape.add_child(shape);
+    strut_shape.add_child(strut_hole);
+
+    let shape = strut_shape;
+
+    let extrude = LinExtrudeParams {
+        height: width,
+        center: true,
+        ..Default::default()
+    };
+
+    let unit: Vector3<f32> = Vector3::new(1.0, 1.0, 1.0);
+    let scaled = scad!(Scale(unit * chord); shape);
+    parts.push(scaled.clone());
+    let strut = scad!(LinearExtrude(extrude); scaled);
+    let rotated = scad!(Rotate(90.0, vec3(1.0, 0.0, 0.0)); strut);
+    Construct {
+        visualization: rotated,
+        parts,
+    }
 }
 
 fn extrude_strut(
@@ -293,26 +307,23 @@ fn lerp(a: f32, b: f32, x: f32) -> f32 {
 
 fn wing(
     aerofoil: &SeligFile,
-    struts: usize,
-    length: f32,
-    chord: f32,
-    taper: f32,
+    config: &WingConfig,
     spar: SparType,
 ) -> ScadObject {
     let mut wing = scad!(Translate(vec3(0.0, 0.0, 0.0)));
 
     // struts
-    for strut_idx in 0..struts + 1 {
-        let gap = length / struts as f32;
+    for strut_idx in 0..config.struts + 1 {
+        let gap = config.length / config.struts as f32;
 
-        let chord = lerp(chord, taper, strut_idx as f32 / struts as f32);
+        let chord = lerp(config.chord, config.chord * config.taper, strut_idx as f32 / config.struts as f32);
 
         let spacing = strut_idx as f32 * gap;
 
         let mut transform = scad!(Translate(vec3(0.0, spacing, 0.0)));
 
         let strut = strut(aerofoil, chord, CARDBOARD_WIDTH, &spar);
-        transform.add_child(strut);
+        transform.add_child(strut.visualization);
         wing.add_child(transform);
     }
 
@@ -372,4 +383,11 @@ fn topwing_spar(
     wing
 }
 
-
+/// Parameters for what would be half of a symmetrical (port/starboard) wing
+/// All distance units are millimeters
+pub struct WingConfig {
+    pub length: f32, /// half of the wingspan
+    pub chord: f32,
+    pub taper: f32, /// chord at wingtip in relation to the chord at the root
+    pub struts: usize,
+}