Update/dash airfoil design

apps/dash-airfoil-design/app.py

@@ -1,11 +1,11 @@
 import plotly.express as px
 import plotly.graph_objects as go
 import dash
-import dash_core_components as dcc
-import dash_html_components as html
+from dash import dcc, html
 import dash_bootstrap_components as dbc
 from dash.dependencies import Input, Output, State
 import aerosandbox as asb
+from aerosandbox.geometry.airfoil.airfoil_families import get_kulfan_coordinates
 import aerosandbox.numpy as np
 import copy
 import plotly.figure_factory as ff
@@ -263,11 +263,10 @@ def display_graph(
 
     ### Start constructing the figure
     airfoil = asb.Airfoil(
-        coordinates=asb.get_kulfan_coordinates(
+        coordinates=get_kulfan_coordinates(
             lower_weights=np.array(kulfan_inputs[n_kulfan_inputs_per_side:]),
             upper_weights=np.array(kulfan_inputs[:n_kulfan_inputs_per_side]),
             TE_thickness=0,
-            enforce_continuous_LE_radius=False,
             n_points_per_side=200,
         )
     )
@@ -351,4 +350,4 @@ def display_graph(
 
 
 if __name__ == "__main__":
-    app.run_server(debug=True)
+    app.run(debug=True)

apps/dash-airfoil-design/app_components.py

@@ -1,5 +1,5 @@
-import dash_core_components as dcc
-import dash_html_components as html
+from dash import dcc, html
+
 
 ### Operating things
 operating_slider_components = [

apps/dash-airfoil-design/pyproject.toml

@@ -0,0 +1,12 @@
+[project]
+name = "dash-airfoil-design"
+version = "0.1.0"
+requires-python = ">=3.12"
+dependencies = [
+    "aerosandbox>=4.2.10",
+    "dash>=4.4.1",
+    "dash-bootstrap-components>=2.0.4",
+    "plotly>=7.0.0",
+    "pandas>=3.0.5",
+    "gunicorn>=26.2.0",
+]

apps/dash-airfoil-design/requirements.txt

@@ -1,7 +1,51 @@
-aerosandbox == 3.0.0 # TODO fix a version
-plotly>= 4.14.3
-dash>= 1.19.0
-dash_core_components>=1.15.0
-dash_html_components>=1.1.2
-dash_bootstrap_components>=0.11.3
-gunicorn
+aerosandbox==4.2.10
+annotated-types==0.8.0
+blinker==1.9.0
+casadi==3.8.0
+certifi==2026.7.22
+charset-normalizer==3.5.1
+click==8.5.0
+colorama==0.4.6 ; sys_platform == 'win32'
+comm==0.2.3
+contourpy==1.3.3
+cycler==0.12.1
+dash==4.4.1
+dash-bootstrap-components==2.0.4
+dill==0.4.1
+flask==3.1.3
+fonttools==4.64.0
+gunicorn==26.2.0
+idna==3.19
+importlib-metadata==9.0.1
+itsdangerous==2.2.0
+janus==2.0.0
+jinja2==3.1.6
+kiwisolver==1.5.1
+markupsafe==3.0.3
+matplotlib==3.11.1
+narwhals==2.25.0
+nest-asyncio==1.6.0
+neuralfoil==0.3.3
+numpy==2.5.3
+packaging==26.3
+pandas==3.0.5
+pillow==12.3.0
+plotly==7.0.0
+pydantic==2.13.5
+pydantic-core==2.46.5
+pyparsing==3.3.2
+python-dateutil==2.9.0.post0
+requests==2.34.2
+retrying==1.4.2
+scipy==1.18.1
+seaborn==0.13.2
+setuptools==84.0.0
+six==1.17.0
+sortedcontainers==2.4.0
+tqdm==4.70.0
+typing-extensions==4.16.0
+typing-inspection==0.4.4
+tzdata==2026.3 ; sys_platform == 'emscripten' or sys_platform == 'win32'
+urllib3==2.7.0
+werkzeug==3.1.8
+zipp==4.1.0

apps/dash-airfoil-design/runtime.txt

@@ -1 +1 @@
-python-3.8.2
+python-3.12.11