Bug fixes and documentation updates (#345)

* Set types on wrap functions * Update IEA-15 inputs * Update installation instructions -- draft * Change to new AF Coords * Fix IEA15 airfoils again * Try latest setup_fortran action * Add UAStart/End location writing * Try intel-classic compiler * Add developer docs about api changes * Try macos-latest in CI * trying to improve conda and pypi builds (#351) * trying to improve conda and pypi builds * adding wheel to cibuild prep * overkill on linux libraries * forgot a step * removing musl aarch64, but don't understand why it fails --------- Co-authored-by: Garrett Barter <[email protected]>
NREL · Jun 10, 2024 · 721164e · 721164e
1 parent 7deb583
commit 721164e
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diff --git a/.github/workflows/CI_rosco-compile.yml b/.github/workflows/CI_rosco-compile.yml
@@ -16,13 +16,15 @@ jobs:
         strategy:
             fail-fast: false #true
             matrix:
-                os: ["ubuntu-latest", "macOS-13", "windows-latest"] #mac-13 intel, mac-14 arm
+                os: ["ubuntu-latest", "macOS-latest", "windows-latest"] #mac-13 intel, mac-14 arm
                 python-version: ["3.9", "3.10", "3.11", "3.12"]
 
         steps:
             - name: Setup GNU Fortran
               if: false == contains( matrix.os, 'windows')
-              uses: awvwgk/setup-fortran@v1 #modflowpy/install-intelfortran-action@v1 #
+              uses: fortran-lang/[email protected]
+              # with:
+              #   compiler: intel-classic
 
             - name: Install compiler
               if: false == contains( matrix.os, 'windows')

diff --git a/.github/workflows/Publish_ROSCO.yml b/.github/workflows/Publish_ROSCO.yml
@@ -12,9 +12,15 @@ jobs:
     strategy:
       fail-fast: false
       matrix:
-        os: [ubuntu-latest, windows-latest, macos-13, macos-14]
+        os: [ubuntu-latest, windows-latest, macos-12, macos-13, macos-14]
 
     steps:
+      - name: Set up QEMU
+        if: runner.os == 'Linux'
+        uses: docker/setup-qemu-action@v3
+        with:
+          platforms: all
+
       - name: Setup GNU Fortran
         if: false == contains( matrix.os, 'windows')
         uses: awvwgk/setup-fortran@v1
@@ -51,16 +57,40 @@ jobs:
       - name: Checkout
         uses: actions/checkout@v4
 
-      - name: Build wheels mac and linux
-        if: false == contains( matrix.os, 'windows')
-        uses: pypa/[email protected]
+      - name: Build wheels linux
+        if: contains( matrix.os, 'ubuntu')
+        uses: pypa/[email protected]
+        env:
+          CC: ${{ steps.install_cc.outputs.cc }}
+          CXX: ${{ steps.install_cc.outputs.cxx }}
+
+      - name: Build wheels mac-12
+        if: contains( matrix.os, 'macos-12')
+        uses: pypa/[email protected]
+        env:
+          CC: ${{ steps.install_cc.outputs.cc }}
+          CXX: ${{ steps.install_cc.outputs.cxx }}
+          CIBW_ENVIRONMENT_MACOS: MACOSX_DEPLOYMENT_TARGET="12.0"
+
+      - name: Build wheels mac-13
+        if: contains( matrix.os, 'macos-13')
+        uses: pypa/[email protected]
+        env:
+          CC: ${{ steps.install_cc.outputs.cc }}
+          CXX: ${{ steps.install_cc.outputs.cxx }}
+          CIBW_ENVIRONMENT_MACOS: MACOSX_DEPLOYMENT_TARGET="13.0"
+
+      - name: Build wheels mac-14
+        if: contains( matrix.os, 'macos-14')
+        uses: pypa/[email protected]
         env:
           CC: ${{ steps.install_cc.outputs.cc }}
           CXX: ${{ steps.install_cc.outputs.cxx }}
+          CIBW_ENVIRONMENT_MACOS: MACOSX_DEPLOYMENT_TARGET="14.0"
 
       - name: Build wheels windows
         if: contains( matrix.os, 'windows')
-        uses: pypa/cibuildwheel@v2.17.0
+        uses: pypa/cibuildwheel@v2.18.1
 
       - uses: actions/upload-artifact@v4
         with:

diff --git a/...-15-240-RWT_AeroDyn15_Polar_00_Coords.txt → ...i/Airfoils/IEA-15-240-RWT_AF00_Coords.txt b/...-15-240-RWT_AeroDyn15_Polar_00_Coords.txt → ...i/Airfoils/IEA-15-240-RWT_AF00_Coords.txt
@@ -2,15 +2,15 @@
 ! ......... x-y coordinates are next if NumCoords > 0 .............
 ! x-y coordinate of airfoil reference
 !  x/c        y/c
-  0.504545        0.
+ 0.500000       0
 ! coordinates of airfoil shape
 ! interpolation to 200 points
 !  x/c        y/c
- 1.00000000000000e+00 -5.22832942930268e-16
+ 1.00000000000000e+00 -5.22829392626822e-16
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@@ -30,7 +30,7 @@
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@@ -46,62 +46,62 @@
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- 3.09878859713640e-03 -5.54780130210999e-02
+ 3.09878859713642e-03 -5.54780130211000e-02
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@@ -194,8 +194,8 @@
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