remove second parameter yaw rate comment

Author: 1-Bart-1

README.md

@@ -114,7 +114,7 @@ wa = BodyAerodynamics([wing])
 
 # Set inflow conditions
 vel_app = [cos(alpha), 0.0, sin(alpha)] .* v_a
-set_va!(wa, (vel_app, 0.0))  # Second parameter is yaw rate
+set_va!(wa, vel_app)
 ```
 It is possible to import the wing geometry using an `.obj` file as shown in the example `ram_air_kite.jl`.
 

docs/src/index.md

@@ -115,7 +115,7 @@ wa = BodyAerodynamics([wing])
 
 # Set inflow conditions
 vel_app = [cos(alpha), 0.0, sin(alpha)] .* v_a
-set_va!(wa, (vel_app, 0.0))  # Second parameter is yaw rate
+set_va!(wa, vel_app)
 ```
 It is possible to import the wing geometry using an `.obj` file as shown in the example `ram_air_kite.jl`.
 

examples/bench.jl

@@ -31,7 +31,7 @@ wa = BodyAerodynamics([wing])
 
 # Set inflow conditions
 vel_app = [cos(alpha), 0.0, sin(alpha)] .* v_a
-set_va!(wa, (vel_app, 0.0))  # Second parameter is yaw rate
+set_va!(wa, vel_app)
 
 # Step 4: Initialize solvers for both LLT and VSM methods
 llt_solver = Solver(aerodynamic_model_type=:LLT)

test/bench.jl

@@ -36,7 +36,7 @@ using LinearAlgebra
     body_aero = BodyAerodynamics([wing])
 
     vel_app = [cos(alpha), 0.0, sin(alpha)] .* v_a
-    set_va!(body_aero, vel_app)  # Second parameter is yaw rate
+    set_va!(body_aero, vel_app)
 
     # Initialize solvers for both LLT and VSM methods
     solver = Solver()

test/test_plotting.jl

@@ -29,7 +29,7 @@ function create_wa()
     wa = BodyAerodynamics([wing])
     # Set inflow conditions
     vel_app = [cos(alpha), 0.0, sin(alpha)] .* v_a
-    set_va!(wa, vel_app)  # Second parameter is yaw rate
+    set_va!(wa, vel_app)
     wa
 end