ank/glider
1
Fork 0
Code Issues Activity

increased main wing taper

Browse source
This commit is contained in:
Andy Killorin 2023-11-01 11:49:18 -05:00
parent 5decd2f570
commit 1f4a2fe8f7
No known key found for this signature in database
GPG key ID: 8CB11B45B690DC2A
2 changed files with 2 additions and 1 deletions
Show stats Download patch file Download diff file Expand all files Collapse all files

1
src/constants.rs
View file

@ -3,6 +3,7 @@
const IN2MM: f32 = 25.4; const IN2MM: f32 = 25.4;
pub const CHORD: f32 = 11.2 * IN2MM; pub const CHORD: f32 = 11.2 * IN2MM;
pub const WING_TAPER: f32 = 0.6;
pub const WINGSPAN: f32 = 45.0 * IN2MM; pub const WINGSPAN: f32 = 45.0 * IN2MM;
pub const LENGTH: f32 = 30.0*IN2MM; pub const LENGTH: f32 = 30.0*IN2MM;
/// strut count in the main wing /// strut count in the main wing

2
src/main.rs
View file

@ -25,7 +25,7 @@ fn main() {
// struts // struts
for port in [true,false] { for port in [true,false] {
let mut wing = wing(&wing_airfoil, STRUTS/2, WINGSPAN/2.0, CHORD, CHORD * 0.8); let mut wing = wing(&wing_airfoil, STRUTS/2, WINGSPAN/2.0, CHORD, CHORD * WING_TAPER);
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);