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test/test_body_aerodynamics.jl
@@ -169,7 +169,7 @@ end
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@test sol.force_coefficients[2] ≈ 0.0 atol=1e-10 # CFy
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@test sol.force_coefficients[3] ≈ 0.49055973654418716 atol=1e-3 # CFz
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@test sol.force_coefficients[3] / sol.force_coefficients[1] ≈ sol.aero_force[3] / sol.aero_force[1]
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- @test sol.moment_distribution[1] ≈ -0.0006683746751654071 atol=1e-10
+ @test sol.moment_distribution[1] ≈ -0.0006683746751654071 atol=1e-8
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@test sol.moment_coefficient_distribution[1] ≈ -2.212405554436003e-7 atol=1e-10
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@test sol.moment_distribution[1] / sol.moment_distribution[2] ≈ sol.moment_coefficient_distribution[1] / sol.moment_coefficient_distribution[2]
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