Merge branch 'main' of https://github.com/cfsengineering/CEASIOMpy

cfsengineering · Jan 29, 2025 · 17a9080 · 17a9080
2 parents a907b03 + 0164a32
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diff --git a/ceasiompy/AeroFrame/runaeroframe.py b/ceasiompy/AeroFrame/runaeroframe.py
@@ -23,7 +23,7 @@
 
 
 TODO:
-    * make working directories
+    * Refactoring
 
 """
 
@@ -55,7 +55,6 @@
 # =================================================================================================
 
 if __name__ == "__main__":
-
     log.info("----- Start of " + MODULE_NAME + " -----")
 
     af.standard_run(args=af.StdRunArgs(dest=DIR_AEROFRAME_WKDIR, verbose=True))

diff --git a/ceasiompy/AeroFrame_new/README.md b/ceasiompy/AeroFrame_new/README.md
@@ -0,0 +1,40 @@
+
+<img align="right" height="70" src="../../documents/logos/CEASIOMpy_banner_main.png">
+
+# ModuleTemplate
+
+**Categories:** Template module, Example, Illustration
+
+**State**: :heavy_check_mark:
+
+This is a template module. Its purpose is to illustrate how other modules of CEASIOMpy should be structured, set up and documented.
+
+<p align="center">
+<img height="160" src="files/Spirit_of_St._Louis.jpg">
+</p>
+
+Example picture. Image in the public domain, from [Wikimedia Commons](https://commons.wikimedia.org/wiki/File:Spirit_of_St._Louis.jpg)
+
+## Inputs
+
+ModuleTemplate needs no inputs.
+
+## Analyses
+
+ModuleTemplate computes nothing.
+
+## Outputs
+
+ModuleTemplate outputs nothing.
+
+## Installation or requirements
+
+ModuleTemplate is a native CEASIOMpy module, hence it is available and installed by default.
+
+## Limitations
+
+ModuleTemplate is limited in every aspect.
+
+## More information
+
+* <https://en.wikipedia.org/wiki/Spirit_of_St._Louis>
diff --git a/ceasiompy/AeroFrame_new/ToolInput/.keep b/ceasiompy/AeroFrame_new/ToolInput/.keep
@@ -0,0 +1 @@
+
diff --git a/ceasiompy/AeroFrame_new/ToolOutput/.keep b/ceasiompy/AeroFrame_new/ToolOutput/.keep
@@ -0,0 +1 @@
+
diff --git a/ceasiompy/AeroFrame_new/__init__.py b/ceasiompy/AeroFrame_new/__init__.py
diff --git a/ceasiompy/AeroFrame_new/__specs__.py b/ceasiompy/AeroFrame_new/__specs__.py
@@ -0,0 +1,215 @@
+from ceasiompy.utils.moduleinterfaces import CPACSInOut
+from ceasiompy.utils.commonxpath import (
+    CEASIOMPY_XPATH,
+    AVL_PLOT_XPATH,
+    AVL_VORTEX_DISTR_XPATH,
+    AVL_AEROMAP_UID_XPATH,
+    AEROPERFORMANCE_XPATH,
+    FRAMAT_MATERIAL_XPATH,
+    FRAMAT_SECTION_XPATH,
+    FRAMAT_MESH_XPATH,
+    AEROFRAME_SETTINGS
+)
+from pathlib import Path
+
+# ===== Module Status =====
+# True if the module is active
+# False if the module is disabled (not working or not ready)
+module_status = True
+
+RESULTS_DIR = Path("Results", "AeroFrame_new")
+
+# ===== CPACS inputs and outputs =====
+
+cpacs_inout = CPACSInOut()
+
+# ----- Input -----
+
+cpacs_inout.add_input(
+    var_name="aeromap_uid",
+    var_type=list,
+    default_value=None,
+    unit=None,
+    descr="Name of the aero map to calculate",
+    xpath=AVL_AEROMAP_UID_XPATH,
+    gui=True,
+    gui_name="__AEROMAP_SELECTION",
+    gui_group="Aeromap settings",
+)
+
+cpacs_inout.add_input(
+    var_name="panel_distribution",
+    var_type=list,
+    default_value=["equal", "cosine", "sine"],
+    unit=None,
+    descr=("Select the type of distribution"),
+    xpath=AVL_VORTEX_DISTR_XPATH + "/Distribution",
+    gui=True,
+    gui_name="Choice of distribution",
+    gui_group="AVL: Vortex Lattice Spacing Distributions",
+)
+
+cpacs_inout.add_input(
+    var_name="chordwise_vort",
+    var_type=int,
+    default_value=8,
+    unit=None,
+    descr="Select the number of chordwise vortices",
+    xpath=AVL_VORTEX_DISTR_XPATH + "/Nchordwise",
+    gui=True,
+    gui_name="Number of chordwise vortices",
+    gui_group="AVL: Vortex Lattice Spacing Distributions",
+)
+
+cpacs_inout.add_input(
+    var_name="spanwise_vort",
+    var_type=int,
+    default_value=30,
+    unit=None,
+    descr="Select the number of spanwise vortices",
+    xpath=AVL_VORTEX_DISTR_XPATH + "/Nspanwise",
+    gui=True,
+    gui_name="Number of spanwise vortices",
+    gui_group="AVL: Vortex Lattice Spacing Distributions",
+)
+
+cpacs_inout.add_input(
+    var_name="save_plots",
+    var_type=bool,
+    default_value=True,
+    unit=None,
+    descr="Select to save geometry and results plots",
+    xpath=AVL_PLOT_XPATH,
+    gui=True,
+    gui_name="Save AVL plots",
+    gui_group="Plots",
+)
+
+cpacs_inout.add_input(
+    var_name="N_beam",
+    var_type=int,
+    default_value=15,
+    unit=None,
+    descr="Enter number of nodes for the beam mesh.",
+    xpath=FRAMAT_MESH_XPATH + "/NumberNodes",
+    gui=True,
+    gui_name="Number of beam nodes",
+    gui_group="FramAT: Mesh properties",
+)
+
+cpacs_inout.add_input(
+    var_name="young_modulus",
+    var_type=float,
+    default_value=70,
+    unit=None,
+    descr="Enter the Young modulus of the wing material in GPa.",
+    xpath=FRAMAT_MATERIAL_XPATH + "/YoungModulus",
+    gui=True,
+    gui_name="Young modulus [GPa]",
+    gui_group="FramAT: Material properties",
+)
+
+cpacs_inout.add_input(
+    var_name="shear_modulus",
+    var_type=float,
+    default_value=26,
+    unit=None,
+    descr="Enter the shear modulus of the wing material in GPa.",
+    xpath=FRAMAT_MATERIAL_XPATH + "/ShearModulus",
+    gui=True,
+    gui_name="Shear modulus [GPa]",
+    gui_group="FramAT: Material properties",
+)
+
+cpacs_inout.add_input(
+    var_name="material_density",
+    var_type=float,
+    default_value=1960,
+    unit=None,
+    descr="Enter the density of the wing material in kg/m³.",
+    xpath=FRAMAT_MATERIAL_XPATH + "/Density",
+    gui=True,
+    gui_name="Material density [kg/m³]",
+    gui_group="FramAT: Material properties",
+)
+
+cpacs_inout.add_input(
+    var_name="cross_section_area",
+    var_type=float,
+    default_value=-1,
+    unit=None,
+    descr="Enter the area of the cross-section in m².",
+    xpath=FRAMAT_SECTION_XPATH + "/Area",
+    gui=True,
+    gui_name="Cross-section area [m²]",
+    gui_group="FramAT: Cross-section properties",
+)
+
+cpacs_inout.add_input(
+    var_name="cross_section_Ix",
+    var_type=float,
+    default_value=-1,
+    unit=None,
+    descr="Enter the second moment of area of the cross-section \
+            about the horizontal axis, in m⁴.",
+    xpath=FRAMAT_SECTION_XPATH + "/Ix",
+    gui=True,
+    gui_name="Second moment of area Ix [m⁴]",
+    gui_group="FramAT: Cross-section properties",
+)
+
+cpacs_inout.add_input(
+    var_name="cross_section_Iy",
+    var_type=float,
+    default_value=-1,
+    unit=None,
+    descr="Enter the second moment of area of the cross-section \
+            about the vertical axis, in m⁴",
+    xpath=FRAMAT_SECTION_XPATH + "/Iy",
+    gui=True,
+    gui_name="Second moment of area Iy [m⁴]",
+    gui_group="FramAT: Cross-section properties",
+)
+
+cpacs_inout.add_input(
+    var_name="n_iter_max",
+    var_type=int,
+    default_value=8,
+    unit=None,
+    descr="Enter the maximum number of iterations of the aeroelastic-loop.",
+    xpath=AEROFRAME_SETTINGS + "/MaxNumberIterations",
+    gui=True,
+    gui_name="Maximum number of iterations",
+    gui_group="AeroFrame: Convergence settings",
+)
+
+cpacs_inout.add_input(
+    var_name="tolerance",
+    var_type=float,
+    default_value=1e-3,
+    unit=None,
+    descr="Enter the tolerance for convergence of the wing deformation.",
+    xpath=AEROFRAME_SETTINGS + "/Tolerance",
+    gui=True,
+    gui_name="Tolerance",
+    gui_group="AeroFrame: Convergence settings",
+)
+
+# ----- Output -----
+
+cpacs_inout.add_output(
+    var_name="output",
+    default_value=None,
+    unit="1",
+    descr="Description of the output",
+    xpath=CEASIOMPY_XPATH + "/test/myOutput",
+)
+
+cpacs_inout.add_output(
+    var_name="aeromap_avl",  # name to change...
+    # var_type=CPACS_aeroMap, # no type pour output, would it be useful?
+    default_value=None,
+    unit="-",
+    descr="aeroMap with aero coefficients calculated by AVL",
+    xpath=AEROPERFORMANCE_XPATH + "/aeroMap/aeroPerformanceMap",
+)