switched to airfoil struct

src/main.rs

@@ -16,10 +16,11 @@ fn main() {
     scad_file.set_detail(50);
 
     // cambered airfoil, used in the wing
-    let wing_airfoil: Airfoil = selig::parse(include_str!("../ag24.dat"));
+    let wing_airfoil: Airfoil = Airfoil::parse(include_str!("../ag24.dat"));
+    println!("perim {}, name {}", wing_airfoil.get_name(), wing_airfoil.perimiter());
 
     // symetric airfoil, used in the control surfaces
-    let control_airfoil: Airfoil = selig::parse(include_str!("../edgevertical.dat"));
+    let control_airfoil: Airfoil = Airfoil::parse(include_str!("../edgevertical.dat"));
 
     let mut wing_transform = scad!(Translate(vec3(0.0,0.0,0.0)));
 
@@ -86,7 +87,7 @@ fn main() {
 
 /// returns a extruded airfoil with the given dimensions
 fn strut(airfoil: &Airfoil, chord: f32, width: f32) -> ScadObject {
-    let aerofoil = scad::PolygonParameters::new(airfoil.clone());
+    let aerofoil = scad::PolygonParameters::new(airfoil.get_points().clone());
     let shape = scad!(Polygon(aerofoil));
 
     let extrude = LinExtrudeParams {

src/selig.rs

@@ -2,16 +2,47 @@ use nalgebra::Vector2;
 
 pub type Point = Vector2<f32>;
 
-pub type Airfoil = Vec<Point>;
-
-pub fn parse(file: &str) -> Airfoil {
-    let mut points = Vec::new();
-
-    for line in file.lines().skip(1) {
-        let mut numbers =line.split(" ").filter(|n| !n.trim().is_empty());
-        let x = numbers.next().unwrap().parse().unwrap();
-        let y = numbers.next().unwrap().parse().unwrap();
-        points.push(Point::new(x,y))
-    }
-    points
+pub struct Airfoil {
+    name: String,
+    data: Vec<Point>,
+}
+
+impl Airfoil {
+    pub fn parse(file: &str) -> Airfoil {
+        let mut points = Vec::new();
+
+        let mut lines = file.lines();
+        let name = lines.next().expect("selig .dat is empty").to_string();
+
+        for line in lines {
+            let mut numbers =line.split(" ").filter(|n| !n.trim().is_empty());
+            let x = numbers.next().unwrap().parse().unwrap();
+            let y = numbers.next().unwrap().parse().unwrap();
+            points.push(Point::new(x,y))
+        }
+        Airfoil {
+            name,
+            data: points
+        }
+    }
+
+    pub fn get_points(&self) -> &Vec<Point> {
+        &self.data
+    }
+
+    pub fn get_name(&self) -> &str {
+        &self.name
+    }
+
+    pub fn perimiter(&self) -> f32 {
+        let mut last_point: Option<Point> = None;
+        let mut distance: f32 = 0.0;
+        for point in self.get_points() {
+            if let Some(last) = last_point {
+                distance += (last - point).magnitude();
+            }
+            last_point = Some(point.clone());
+        }
+        distance
+    }
 }