From c1a3e2a1ada80c6b449e7d4398259dc6dd0ef7c3 Mon Sep 17 00:00:00 2001 From: Alasdair Gray Date: Mon, 15 Jul 2024 20:34:11 -0400 Subject: [PATCH] Remove commented out old code --- .../test_aerostruct_wingbox_wave_fuel_vol_constraint_opt.py | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/openaerostruct/tests/test_aerostruct_wingbox_wave_fuel_vol_constraint_opt.py b/openaerostruct/tests/test_aerostruct_wingbox_wave_fuel_vol_constraint_opt.py index ae783b961..c4178a26b 100644 --- a/openaerostruct/tests/test_aerostruct_wingbox_wave_fuel_vol_constraint_opt.py +++ b/openaerostruct/tests/test_aerostruct_wingbox_wave_fuel_vol_constraint_opt.py @@ -289,7 +289,7 @@ def test(self): # Airfoil properties for viscous drag calculation "k_lam": 0.05, # percentage of chord with laminar # flow, used for viscous drag - "t_over_c_cp": 0.12 * np.ones(6), # np.array([0.08, 0.08, 0.08, 0.10, 0.10, 0.12]), + "t_over_c_cp": 0.12 * np.ones(6), "original_wingbox_airfoil_t_over_c": 0.12, "c_max_t": 0.38, # chordwise location of maximum thickness "with_viscous": True,