MRG: Merge pull request #3 from aerosense-ai/feature/improve-geometry…

…-file-handling

Feature: Improve geometry file handling

app.py

@@ -14,11 +14,11 @@ def run(analysis):
     if analysis.configuration_values['analysis_program'] == 'xfoil':
         xfoil_module.call(analysis)  # Pass the parsed input and configuration schema
     elif analysis.configuration_values['analysis_program'] == 'vgfoil':
-        pass
+        raise NotImplementedError("Vortex Generator XFOIL is not implemented yet!")
     elif analysis.configuration_values['analysis_program'] == 'viiflow':
-        pass
+        raise NotImplementedError("VIIFLOW is not implemented!")
     elif analysis.config['analysis_program'] == 'rfoil':
-        pass
+        raise NotImplementedError("RFOIL by DTU is not implemented!")
 
     analysis.finalise()
 

app_configuration.json

@@ -1,6 +1,7 @@
 {
   "configuration_values": {
     "analysis_program": "xfoil",
+    "silent_mode": true,
     "max_iterations":1000,
     "backend": {
         "name": "GCPPubSubBackend",

pyproject.toml

@@ -1,6 +1,6 @@
 [tool.poetry]
 name = "panel-codes-service"
-version = "0.0.1"
+version = "0.1.0"
 description = ""
 authors = ["time-trader"]
 license = "MIT"

tests/test_deployment.py

@@ -17,19 +17,19 @@ def test_deployment(self):
         )
 
         input_values = {
-            "airfoil_label": "naca-0012",
-            "alpha_range": [-10, 10, 3],
+            "airfoil_geometry": {"airfoil_geometry_filename": "naca_0012.dat"},
+            "alpha_range": [0, 6, 3],
             "repanel": False,
-            "inflow_speed": 1,
-            "kinematic_viscosity": 1e-6,
+            "inflow_speed": 100,
+            "kinematic_viscosity": 15e-6,
             "characteristic_length": 1,
-            "mach_number": 0,
+            "mach_number": 0.3,
             "n_critical": 9,
             "re_xtr": [5e5, 5e5]
         }
 
         child = Child(
-            id="aerosense/panel-codes:0.0.1",
+            id="aerosense/panel-codes:0.1.0",
             backend={"name": "GCPPubSubBackend", "project_name": "aerosense-twined"},
         )
 

tests/xfoil/cases/geometry_files/naca_0012.dat

@@ -0,0 +1,100 @@
+NACA 0012
+1.0 0.001259999999999961
+0.9989726963751682 0.0014040493416585976
+0.995895006911623 0.0018345117033156443
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+0.9504844339512095 0.008001602738627567
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+0.8117449009293667 0.024921098885267084
+0.7860583300610847 0.02776246754545424
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+0.0 0.0
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+1.0 -0.001259999999999961

tests/xfoil/cases/naca0012/configuration_values.json

@@ -0,0 +1,9 @@
+{
+    "analysis_program": "xfoil",
+    "silent_mode": true,
+    "max_iterations":1000,
+    "backend": {
+        "name": "GCPPubSubBackend",
+        "project_name": "aerosense-twined"
+    }
+}