From 3e79dbda7e763d5bfe874212a73e83643517bc14 Mon Sep 17 00:00:00 2001
From: Nicolas Gomez <ngomezve@mit.edu>
Date: Mon, 10 Jun 2024 16:51:23 -0400
Subject: [PATCH] eliminated parm from update fun

---
 src/IO/read_input.jl          | 2 +-
 src/structures/update_fuse.jl | 5 ++---
 test/unit_test_structures.jl  | 1 -
 3 files changed, 3 insertions(+), 5 deletions(-)

diff --git a/src/IO/read_input.jl b/src/IO/read_input.jl
index d7d57d11..5fe91f9f 100644
--- a/src/IO/read_input.jl
+++ b/src/IO/read_input.jl
@@ -619,7 +619,7 @@ readvtail(x) = read_input(x, vtail, dvtail)
 if calculate_cabin #Resize the cabin if desired, keeping deltas
     @info "Fuselage and stabilizer layouts have been overwritten; deltas will be maintained."
 
-    update_fuse_for_pax!(pari, parg, parm, fuse_tank) #update fuselage dimensions
+    update_fuse_for_pax!(pari, parg, fuse_tank) #update fuselage dimensions
 end
 # ---------------------------------
 
diff --git a/src/structures/update_fuse.jl b/src/structures/update_fuse.jl
index 2ab75fd0..2dbc8c5a 100644
--- a/src/structures/update_fuse.jl
+++ b/src/structures/update_fuse.jl
@@ -52,7 +52,7 @@ function update_fuse!(pari, parg)
 end
 
 """
-    update_fuse_for_pax!(pari, parg, parm, fuse_tank)
+    update_fuse_for_pax!(pari, parg, fuse_tank)
 
 Function to update the fuselage layout when the cabin length is not known a priori, for example if the radius is changed. 
 It sizes the cabin for the design number of passengers.
@@ -61,13 +61,12 @@ It sizes the cabin for the design number of passengers.
     **Inputs:**
     - `pari::Vector{Int64}`: vector with aircraft integer parameters
     - `parg::Vector{Float64}`: vector with aircraft geometric and mass parameters
-    - `parm::Array{Float64}`: array with mission parameters
     - `fuse_tank::struct`: structure of type `fuselage_tank` with cryogenic fuel tank parameters
 
     **Outputs:**
     No direct outputs; parameters in `parg` are modified.
 """
-function update_fuse_for_pax!(pari, parg, parm, fuse_tank)
+function update_fuse_for_pax!(pari, parg, fuse_tank)
 
     seat_pitch = parg[igseatpitch]
     seat_width = parg[igseatwidth]
diff --git a/test/unit_test_structures.jl b/test/unit_test_structures.jl
index 86b504a4..14bbec78 100644
--- a/test/unit_test_structures.jl
+++ b/test/unit_test_structures.jl
@@ -1,4 +1,3 @@
-
 @testset "structural components" begin
 
 # Fuselage weight