fix test typos

src/C4Blade/airfoil_corrections.jl

@@ -1,4 +1,3 @@
-
 ######################################################################
 #                                                                    #
 #                       Robustness Adjustments                       #

test/afcorrections.jl

@@ -5,7 +5,7 @@ println("\nAIRFOIL CORRECTION TESTS")
     include("data/naca_4412_raw.jl")
 
     # apply stall cutoffs
-    clext, cdext = dt.c4b.stalllimiters(alpha, cl, cdrag; cutoff_slope=0.1, N=20, blend_hardness=50)
+    clext, cdext = dt.c4b.stall_limiters(alpha, cl, cdrag; cutoff_slope=0.1, N=20, blend_hardness=50)
 
     @test ismonotonic(clext, 1)
 end
@@ -20,7 +20,7 @@ end
     stagger = oneoversig05[:, 1] * pi / 180.0
     for (i, s) in enumerate(stagger)
         @test isapprox(
-            oneoversig05[i, 2], dt.c4b.solidityandstaggerfactorsmooth(solidity, s), atol=1e-2
+            oneoversig05[i, 2], dt.c4b.solidity_and_stagger_factor_smooth(solidity, s), atol=1e-2
         )
     end
 
@@ -29,7 +29,7 @@ end
     stagger = oneoversig10[:, 1] * pi / 180.0
     for (i, s) in enumerate(stagger)
         @test isapprox(
-            oneoversig10[i, 2], dt.c4b.solidityandstaggerfactorsmooth(solidity, s), atol=1e-2
+            oneoversig10[i, 2], dt.c4b.solidity_and_stagger_factor_smooth(solidity, s), atol=1e-2
         )
     end
 
@@ -38,46 +38,46 @@ end
     stagger = oneoversig15[:, 1] * pi / 180.0
     for (i, s) in enumerate(stagger)
         @test isapprox(
-            oneoversig15[i, 2], dt.c4b.solidityandstaggerfactorsmooth(solidity, s), atol=1e-2
+            oneoversig15[i, 2], dt.c4b.solidity_and_stagger_factor_smooth(solidity, s), atol=1e-2
         )
     end
 
     # check that factor is constant below 20 degrees
     solidity = 2.0
     @test isapprox(
-        dt.c4b.solidityandstaggerfactorsmooth(solidity, 10.0 * pi / 180),
-        dt.c4b.solidityandstaggerfactorsmooth(solidity, 11.0 * pi / 180),
+        dt.c4b.solidity_and_stagger_factor_smooth(solidity, 10.0 * pi / 180),
+        dt.c4b.solidity_and_stagger_factor_smooth(solidity, 11.0 * pi / 180),
         atol=1e-8,
     )
 
     # check that factor maxes out at 1.0
-    @test 1.0 == dt.c4b.solidityandstaggerfactorsmooth(0.5, 80.0 * pi / 180)
+    @test 1.0 == dt.c4b.solidity_and_stagger_factor_smooth(0.5, 80.0 * pi / 180)
 end
 
 @testset "Prandtl-Glauert Compressibility Corrections" begin
     # - Check that things aren't weird - #
-    @test dt.c4b.prandtlglauertfactor(0.1) == 1.0 / sqrt(1.0 - 0.1^2)
+    @test dt.c4b.prandtl_glauert_factor(0.1) == 1.0 / sqrt(1.0 - 0.1^2)
 
     # - Check that M=1 doesn't break - #
-    @test !isinf(dt.c4b.prandtlglauertfactor(1.0))
+    @test !isinf(dt.c4b.prandtl_glauert_factor(1.0))
 
     # - Check that M>1 doesn't break - #
-    @test isreal(dt.c4b.prandtlglauertfactor(2.0))
+    @test isreal(dt.c4b.prandtl_glauert_factor(2.0))
 
     # - Check that M>1 behavior is as expected - #
-    @test dt.c4b.prandtlglauertfactor(1.1) == 1.0 / sqrt(1.0 - 0.99^2)
+    @test dt.c4b.prandtl_glauert_factor(1.1) == 1.0 / sqrt(1.0 - 0.99^2)
 end
 
 @testset "Reynolds Number Corrections" begin
     # - check that nothing is weird - #
-    @test dt.c4b.redrag(1.0, 2e6, 5e6; reexp=0.5) == (5e6 / 2e6)^0.5
+    @test dt.c4b.re_drag(1.0, 2e6, 5e6; re_exp=0.5) == (5e6 / 2e6)^0.5
 end
 
 @testset "Transonic Effects Corrections" begin
 
     # - Check that lift is being limited after critical mach - #
     @test all(
-        dt.c4b.transonicliftlimitersmooth!([-1.0, 1.0], 0.9, 0.1, 1.0, -1.0, 2 * pi) .< [1.0]
+        dt.c4b.transonic_lift_limiter_smooth!([-1.0, 1.0], 0.9, 0.1, 1.0, -1.0, 2 * pi) .< [1.0]
     )
-    @test all(dt.c4b.transonicliftlimitersmooth!([-1.0], 0.9, 0.1, 1.0, -1.0, 2 * pi) .> [-1.0])
+    @test all(dt.c4b.transonic_lift_limiter_smooth!([-1.0], 0.9, 0.1, 1.0, -1.0, 2 * pi) .> [-1.0])
 end