New test files

src/test/test-1095-e423-eppler-to-profoil-conversion.in

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+AIRFOIL test-1095-e423-eppler-to-profoil-conversion
+# Conversion of Eppler's TRA data to a PROFOIL file.
+# Ref: Eppler, R, "Airfoil Design and Data", Springer-Verlag, 1990, p304, p554
+# If using this file for design, file "test-1095-e423-profoil-conversion.in" is a better starting point.
+
+#SKIP_UNKNOWN_WORDS
+
+COORD 60
+FOIL  16.4  18.7         16.4  18.7 
+FOIL  18.4   3            2     3 
+FOIL  20.4  10            2    10 
+FOIL  21.5  14.7          1.1  14.7 
+FOIL  23.5  15.3          2    15.3 
+FOIL  25.5  16.2          2    16.2 
+FOIL  27.5  17.4          2    17.4
+FOIL  29.5  18.9          2    18.9 
+FOIL  31.5  20.7          2    20.7 
+FOIL  34.72364   23.2     0    23.2 
+FOIL  36.5  10           36.5  10 
+FOIL  38.5  12            2    12 
+FOIL  40.5  15            2    15 
+FOIL  45.5  19            5    19 
+FOIL  50.5  11            5    11 
+FOIL  55     3       
+FOIL  60     3           60     3
+PHIS 5  55
+REC  1  0.00000001
+VLEV 1  1.2
+ILE 10
+
+
+# Use a cubic spline to find the maximum point for normalization to unit chord.
+NORMALIZATION_METHOD 2
+# Slightly rotate normalized airfoil to better match Eppler original airfoil.
+ALFA0_BUMP 0.12
+
+TOLSPEC 0.00001
+ITERMAX 40
+NOECHO
+
+# spec KS
+NEWT1G0 100 1.0 1 10
+IDES
+
+
+# spec mu u.s. and mu l.s.
+NEWT1G0 190 1.0   4   1  0.1
+NEWT1G0 191 0.0   6 100  0.5 
+IDES
+
+# spec omega u.s.
+NEWT1G0 194 .66   7   100  0.1
+IDES
+
+# spec t/c max
+NEWT1G0  107 .1234 6 200 .5 
+IDES
+
+
+#--------------------------------------------------
+# Evaluate moment and camber.  Do not iterate.
+TOLSPEC 100
+ITERMAX 0
+NOECHO
+NEWT1G0 101  0.0  4 1 0.1
+NEWT1G0 105  0.0  4 1 0.1
+IDES
+# Cmo    = -0.26653  ... from 101
+# camber =  0.10034  ... from 105
+# K upper = 0.38383  ... from converged dump file
+#--------------------------------------------------
+
+
+FINISH 100
+ALFASP 2
+14
+18
+VELDIST 60
+DUMP
+
+*
+

src/test/test-1096-e423-profoil-conversion.in

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+AIRFOIL test-1096-e423-profoil-conversion
+# Generated from "test-e423-eppler-to-profoil-conversion.in" and its output.
+
+#SKIP_UNKNOWN_WORDS
+
+COORD 60
+FOIL    16.40000    18.62533    1
+FOIL    18.40000     2.92533    2
+FOIL    20.40000     9.92533    3
+FOIL    21.50000    14.62533    4
+FOIL    23.50000    15.22533    5
+FOIL    25.50000    16.12533    6
+FOIL    27.50000    17.32533    7
+FOIL    29.50000    18.82533    8
+FOIL    31.50000    20.62533    9
+FOIL    34.72364    23.12533   10
+FOIL    36.50000     9.66425   11
+FOIL    38.50000    11.66425   12
+FOIL    40.50000    14.66425   13
+FOIL    45.50000    18.66425   14
+FOIL    50.50000    10.66425   15
+FOIL    55.00000     2.66425   16
+FOIL    60.00000     2.66425   17
+PHIS     5.00000    55.00000
+REC      0.38383     0.00000001
+VLEV     1           1.70640
+ILE     10
+
+
+# Use a cubic spline to find the maximum point for normalization to unit chord.
+NORMALIZATION_METHOD 2
+# Comment out next line if using this file as a starting point for a new design.
+ALFA0_BUMP 0.12
+
+TOLSPEC 0.00001
+ITERMAX 40
+NOECHO
+
+# spec KS
+NEWT1G0 100 1.0 1 10
+IDES
+
+# spec Cmo
+NEWT1G0 101 -0.26653  4 1 0.1
+IDES
+
+# spec t/c max
+NEWT1G0  107 .1234 6 300 .5 
+IDES
+
+
+
+
+FINISH 100
+ALFASP 2
+14
+18
+VELDIST 60
+DUMP
+
+*
+