eliminated parm from update fun

MIT-LAE · Jun 10, 2024 · 3e79dbd · 3e79dbd
1 parent 01ff3ee
commit 3e79dbd
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Showing 3 changed files with 3 additions and 5 deletions.
diff --git 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
@@ -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
@@ -1,4 +1,3 @@
-
 @testset "structural components" begin
 
 # Fuselage weight