Load elevator airfoil separately

Makefile

@@ -1,5 +1,6 @@
-MAIN_AIRFOIL    = ag24.dat
-CONTROL_AIRFOIL = m1-il.dat
+MAIN_AIRFOIL     = ag41d
+ELEVATOR_AIRFOIL = b540ols-il
+RUDDER_AIRFOIL   = ht13
 TAIL             = t-tail
 
 UNAME = $(shell uname)
@@ -10,7 +11,7 @@ ifeq ($(UNAME), Darwin)
 	SCAD = OpenSCAD
 endif
 
-AIRFOILS = $(MAIN_AIRFOIL) $(CONTROL_AIRFOIL)
+AIRFOILS = $(MAIN_AIRFOIL).dat $(ELEVATOR_AIRFOIL).dat $(RUDDER_AIRFOIL).dat
 
 b: build/allparts.svg
 
@@ -35,6 +36,9 @@ e393.dat:
 ag24.dat:
 	curl https://m-selig.ae.illinois.edu/ads/coord/ag24.dat -o ag24.dat
 
+ag41d.dat:
+	curl https://web.mit.edu/drela/Public/web/avl/runs/ag41d.dat -o $@
+
 sd8020.dat:
 	curl http://airfoiltools.com/airfoil/seligdatfile?airfoil=sd8020-il -o $@
 
@@ -88,7 +92,7 @@ build/testwing-clear.scad: build/testwing.scad
 	sed 's/color("clear-red")/color([1.0,1.0,0.0,0.9])/g' $< > $@
 	sed 's/color("clear-blue")/color([0.0,1.0,1.0,1.0])/g' -i $@
 
-build/assembly-clear.scad: src/*.rs $(AIRFOILS)
+build/assembly-clear.scad: src/*.rs $(AIRFOILS) build
 	cargo run $(AIRFOILS) assembly $(TAIL) film stdout |\
 	sed 's/color("clear-red")/color([1.0,0.0,0.0,0.5])/g' |\
 	sed 's/color("clear-blue")/color([0.0,1.0,0.0,0.9])/g' |\

src/main.rs

@@ -13,8 +13,10 @@ fn main() {
     let mut args = args().skip(1);
     let main_airfoil_path = args.next().unwrap();
     let main_airfoil_path = Path::new(&main_airfoil_path);
-    let control_airfoil_path = args.next().unwrap();
-    let control_airfoil_path = Path::new(&control_airfoil_path);
+    let elevator_airfoil_path = args.next().unwrap();
+    let elevator_airfoil_path = Path::new(&elevator_airfoil_path);
+    let rudder_airfoil_path = args.next().unwrap();
+    let rudder_airfoil_path = Path::new(&rudder_airfoil_path);
     let args: Vec<String> = args.collect();
     let gen_film = args.contains(&"film".to_string());
     let gen_v_tail = args.contains(&"v-tail".to_string());
@@ -37,10 +39,16 @@ fn main() {
         eprintln!("{}", desc);
     }
 
-    // symmetric airfoil, used in the control surfaces
-    let control_airfoil: SeligFile = SeligFile::load(control_airfoil_path).unwrap();
-    eprintln!("Control airfoil: {}", control_airfoil.get_name());
-    if let Some(desc) = control_airfoil.get_description() {
+    // symmetric airfoil
+    let rudder_airfoil: SeligFile = SeligFile::load(rudder_airfoil_path).unwrap();
+    eprintln!("Rudder airfoil: {}", rudder_airfoil.get_name());
+    if let Some(desc) = rudder_airfoil.get_description() {
+        eprintln!("{}", desc);
+    }
+
+    let elevator_airfoil: SeligFile = SeligFile::load(elevator_airfoil_path).unwrap();
+    eprintln!("Elevator airfoil: {}", elevator_airfoil.get_name());
+    if let Some(desc) = elevator_airfoil.get_description() {
         eprintln!("{}", desc);
     }
 
@@ -65,19 +73,19 @@ fn main() {
 
     if gen_t_tail {
         t_tail(
-            &control_airfoil,
+            &rudder_airfoil,
             &mut parts,
             &mut scad_file,
-            &wing_airfoil,
+            &elevator_airfoil,
             gen_film,
         );
     }
     if gen_v_tail {
         v_tail(
-            &control_airfoil,
+            &rudder_airfoil,
             &mut parts,
             &mut scad_file,
-            &wing_airfoil,
+            &elevator_airfoil,
             gen_film,
         );
     }