fix blemishes and remove bad foils

peterdsharpe · Feb 19, 2024 · a23ff22 · a23ff22
1 parent 6b82927
commit a23ff22
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Showing 27 changed files with 1 addition and 470 deletions.
diff --git a/aerosandbox/geometry/airfoil/airfoil_database/ah81k144wfKlappe.dat b/aerosandbox/geometry/airfoil/airfoil_database/ah81k144wfKlappe.dat
@@ -95,4 +95,3 @@ AH 81-K-144 W-F KLAPPE
 0.99039     -0.00467
 0.99572     -0.00433
 0.99893     -0.00400
-1.00000     0.00000
diff --git a/aerosandbox/geometry/airfoil/airfoil_database/ah93w480b.dat b/aerosandbox/geometry/airfoil/airfoil_database/ah93w480b.dat
@@ -1,7 +1,6 @@
 AH 93-W-480B
 1.00000   0.10990
 0.99991   0.11047
-0.99702   0.12519
 0.99467   0.12550
 0.99156   0.12944
 0.98761   0.13418

diff --git a/aerosandbox/geometry/airfoil/airfoil_database/bacj.dat b/aerosandbox/geometry/airfoil/airfoil_database/bacj.dat
@@ -98,4 +98,3 @@ BOEING AIRFOIL J
 0.979999 0.001491
 0.990000 0.000610
 1.000000 -0.000410
-1.000000 0.000950
diff --git a/aerosandbox/geometry/airfoil/airfoil_database/bw050209.dat b/aerosandbox/geometry/airfoil/airfoil_database/bw050209.dat
@@ -1,6 +1,5 @@
 BW 05 02 09
 1.00000 0.00000
-0.99999 0.00100
 0.95000 0.00450
 0.90000 0.00813
 0.80000 0.01833
@@ -44,5 +43,4 @@ BW 05 02 09
 0.80000 -0.02184
 0.90000 -0.01400
 0.95000 -0.00777
-0.99999 -0.00100
 1.00000 0.00000
diff --git a/aerosandbox/geometry/airfoil/airfoil_database/clarkk.dat b/aerosandbox/geometry/airfoil/airfoil_database/clarkk.dat
diff --git a/aerosandbox/geometry/airfoil/airfoil_database/fx049915.dat b/aerosandbox/geometry/airfoil/airfoil_database/fx049915.dat
diff --git a/aerosandbox/geometry/airfoil/airfoil_database/fx057816.dat b/aerosandbox/geometry/airfoil/airfoil_database/fx057816.dat
diff --git a/aerosandbox/geometry/airfoil/airfoil_database/fx082512.dat b/aerosandbox/geometry/airfoil/airfoil_database/fx082512.dat
diff --git a/aerosandbox/geometry/airfoil/airfoil_database/fx69274.dat b/aerosandbox/geometry/airfoil/airfoil_database/fx69274.dat
@@ -94,5 +94,4 @@ FX 69-274
 0.98296     -0.00819
 0.99039     -0.00757
 0.99572     -0.00711
-0.99893     -0.00686
 1.00000     0.00000
diff --git a/aerosandbox/geometry/airfoil/airfoil_database/fx73170.dat b/aerosandbox/geometry/airfoil/airfoil_database/fx73170.dat
@@ -94,5 +94,4 @@ FX 73-170
 0.98296     0.00162
 0.99039     0.00057
 0.99572     -0.00016
-0.99893     -0.00081
 1.00000     0.00000
diff --git a/aerosandbox/geometry/airfoil/airfoil_database/fx73170a.dat b/aerosandbox/geometry/airfoil/airfoil_database/fx73170a.dat
@@ -94,5 +94,4 @@ FX 73-170 A
 0.98296     0.00040
 0.99039     -0.00022
 0.99572     -0.00060
-0.99893     -0.00091
 1.00000     0.00000
diff --git a/aerosandbox/geometry/airfoil/airfoil_database/fx73k170.dat b/aerosandbox/geometry/airfoil/airfoil_database/fx73k170.dat
@@ -94,5 +94,4 @@ FX 73-K-170/22
 0.98296     0.00146
 0.99039     0.00049
 0.99572     -0.00020
-0.99893     -0.00082
 1.00000     0.00000
diff --git a/aerosandbox/geometry/airfoil/airfoil_database/goe477.dat b/aerosandbox/geometry/airfoil/airfoil_database/goe477.dat
diff --git a/aerosandbox/geometry/airfoil/airfoil_database/goe480.dat b/aerosandbox/geometry/airfoil/airfoil_database/goe480.dat
diff --git a/aerosandbox/geometry/airfoil/airfoil_database/goe507.dat b/aerosandbox/geometry/airfoil/airfoil_database/goe507.dat
diff --git a/aerosandbox/geometry/airfoil/airfoil_database/goe517.dat b/aerosandbox/geometry/airfoil/airfoil_database/goe517.dat
diff --git a/aerosandbox/geometry/airfoil/airfoil_database/goe584.dat b/aerosandbox/geometry/airfoil/airfoil_database/goe584.dat
diff --git a/aerosandbox/geometry/airfoil/airfoil_database/m7.dat b/aerosandbox/geometry/airfoil/airfoil_database/m7.dat
diff --git a/aerosandbox/geometry/airfoil/airfoil_database/naca16006.dat b/aerosandbox/geometry/airfoil/airfoil_database/naca16006.dat
diff --git a/aerosandbox/geometry/airfoil/airfoil_database/naca6412.dat b/aerosandbox/geometry/airfoil/airfoil_database/naca6412.dat
@@ -59,5 +59,4 @@ NACA 6412
      0.97465   0.00024
      0.98854  -0.00057
      0.99694  -0.00107
-     0.99975  -0.00124
-     1.00000   0.00000
+     1.00000  -0.00124