one more fix

ufechner7 · ufechner7 · commit b5295d5dca13 · 2025-02-26T17:06:38.000+01:00
diff --git a/examples/bench.jl b/examples/bench.jl
@@ -55,7 +55,7 @@ wing = KiteWing("data/ram_air_kite_body.obj", "data/ram_air_kite_foil.dat")
 body_aero = BodyAerodynamics([wing])
 
 # Create solvers
-VSM_solver = Solver(
+vsm_solver = Solver(
     aerodynamic_model_type=VSM,
     is_with_artificial_damping=false
 )
@@ -74,8 +74,8 @@ vel_app = [
 set_va!(body_aero, vel_app)
 
 # Solving and plotting distributions
-results = solve(VSM_solver, body_aero)
+results = solve(vsm_solver, body_aero)
 println("RAM-air kite:")
-@time results = solve(VSM_solver, body_aero)
+@time results = solve(vsm_solver, body_aero)
 
 nothing
diff --git a/examples/ram_air_kite.jl b/examples/ram_air_kite.jl
@@ -16,7 +16,7 @@ wing = KiteWing("data/ram_air_kite_body.obj", "data/ram_air_kite_foil.dat")
 body_aero = BodyAerodynamics([wing])
 
 # Create solvers
-VSM = Solver(
+vsm_solver = Solver(
     aerodynamic_model_type=VSM,
     is_with_artificial_damping=false
 )
@@ -47,8 +47,8 @@ plot && plot_geometry(
 )
 
 # Solving and plotting distributions
-results = solve(VSM, body_aero)
-@time results = solve(VSM, body_aero)
+results = solve(vsm_solver, body_aero)
+@time results = solve(vsm_solver, body_aero)
 
 body_y_coordinates = [panel.aero_center[2] for panel in body_aero.panels]
 
@@ -63,7 +63,7 @@ plot && plot_distribution(
 )
 
 plot && plot_polars(
-    [VSM],
+    [vsm_solver],
     [body_aero],
     [
         "VSM from Ram Air Kite OBJ and DAT file",

Original file line number	Diff line number	Diff line change
`@@ -16,7 +16,7 @@ wing = KiteWing("data/ram_air_kite_body.obj", "data/ram_air_kite_foil.dat")`
`16`	`16`	`body_aero = BodyAerodynamics([wing])`
`17`	`17`
`18`	`18`	`# Create solvers`
`19`		`-VSM = Solver(`
	`19`	`+vsm_solver = Solver(`
`20`	`20`	`aerodynamic_model_type=VSM,`
`21`	`21`	`is_with_artificial_damping=false`
`22`	`22`	`)`
`@@ -47,8 +47,8 @@ plot && plot_geometry(`
`47`	`47`	`)`
`48`	`48`
`49`	`49`	`# Solving and plotting distributions`
`50`		`-results = solve(VSM, body_aero)`
`51`		`-@time results = solve(VSM, body_aero)`
	`50`	`+results = solve(vsm_solver, body_aero)`
	`51`	`+@time results = solve(vsm_solver, body_aero)`
`52`	`52`
`53`	`53`	`body_y_coordinates = [panel.aero_center[2] for panel in body_aero.panels]`
`54`	`54`
`@@ -63,7 +63,7 @@ plot && plot_distribution(`
`63`	`63`	`)`
`64`	`64`
`65`	`65`	`plot && plot_polars(`
`66`		`- [VSM],`
	`66`	`+ [vsm_solver],`
`67`	`67`	`[body_aero],`
`68`	`68`	`[`
`69`	`69`	`"VSM from Ram Air Kite OBJ and DAT file",`