183 create a load geometry from yaml function for vortexstepmethodjl and run on a simple wing

data/TUDELFT_V3_KITE/wing_geometry_polars_CFD.yaml → data/TUDELFT_V3_KITE/aero_geometry.yaml

@@ -104,130 +104,4 @@ wing_airfoils:
     - [16, polars, {csv_file_path: "polars_CFD/16.csv"}]
     - [17, polars, {csv_file_path: "polars_CFD/17.csv"}]
     - [18, polars, {csv_file_path: "polars_CFD/18.csv"}]
-    - [19, polars, {csv_file_path: "polars_CFD/19.csv"}]
-
-
-
-bridle_nodes:
-  # ---------------------------------------------------------------
-  # headers:
-  #   - id: integer, unique identifier for the node
-  #   - x: x-coordinate [m]
-  #   - y: y-coordinate [m]
-  #   - z: z-coordinate [m]
-  #   - type: node type, either 'knot' or 'pulley'
-  # ---------------------------------------------------------------
-  headers: [id, x, y, z, type]
-  data:
-    - [21, -0.67653494, 2.10580567, 7.08413599, knot]
-    - [22, -0.79196791, 1.01882151, 7.57069579, knot]
-    - [23, -0.79196791, -1.01882151, 7.57069579, knot]
-    - [24, -0.67653494, -2.10580567, 7.08413599, knot]
-    - [25, -0.46444477, 0.77505128, 4.23316161, knot]
-    - [26, -0.46444477, -0.77505128, 4.23316161, knot]
-    - [27, 0.54344694, 1.57655435, 5.91086207, knot]
-    - [28, 0.62960591, 0.92728966, 6.64639402, knot]
-    - [29, 0.62960591, -0.92728966, 6.64639402, knot]
-    - [30, 0.54344694, -1.57655435, 5.91086207, knot]
-    - [31, 0.39092886, 0.71221536, 4.26118728, knot]
-    - [32, 0.39092886, -0.71221536, 4.26118728, knot]
-    - [33, 0.30679124, 0.49235914, 3.39885672, pulley]
-    - [34, 0.28625931, 0.0, 3.19030736, knot]
-    - [35, 0.30679124, -0.49235914, 3.39885672, pulley]
-    - [36, 0.13269336, 0.23394851, 1.48060245, knot]
-    - [37, 0.13269336, -0.23394851, 1.48060245, knot]
-
-bridle_lines:
-  # ---------------------------------------------------------------
-  # headers:
-  #   - name: string, line name
-  #   - rest_length: measured rest length [m]
-  #   - diameter: line diameter [m]
-  #   - material: string, material type (e.g., dyneema)
-  #   - density: material density [kg/m^3]
-  # ---------------------------------------------------------------
-  headers: [name, rest_length, diameter, material, density]
-  data:
-  # front lines
-  - [a6, 11.790, 0.002, dyneema,970]
-  - [A5, 2.870, 0.002, dyneema,970]
-  - [A3, 3.450, 0.002, dyneema,970]
-  - [A2, 3.500, 0.002, dyneema,970]
-  - [A1, 3.690, 0.002, dyneema,970]
-  - [AII, 3.250, 0.002, dyneema,970]
-  - [AI, 3.620, 0.002, dyneema,970]
-  - [amain, 3.910, 0.002, dyneema,970]
-  # rear lines
-  - [br1, 4.410, 0.002, dyneema,970]
-  - [br2, 4.170, 0.002, dyneema,970]
-  - [br3, 4.140, 0.002, dyneema,970]
-  - [br5, 3.580, 0.002, dyneema,970]
-  - [br6, 13.560, 0.002, dyneema,970]
-  - [BRI, 2.360, 0.002, dyneema,970]
-  - [BRII, 2.080, 0.002, dyneema,970]
-  - [BR-main-1, .700, 0.002, dyneema,970]
-  - [M-line, 2.410, 0.002, dyneema,970]
-  # - [S, 1.730, 0.002, dyneema,970] # measured
-  # - [Power Tape, 3.330, 0.002, polyester] # measured
-  - [Steering Tape, 1.530, 0.002, dyneema,970] # trying 0.2m smalller
-  - [Power Tape, 2.900, 0.002, dyneema,970] # trying 0.2m smaller
-
-bridle_connections:
-  # ---------------------------------------------------------------
-  # headers:
-  #   - name: string, line name
-  #   - ci: integer, node id (start)
-  #   - cj: integer, node id (end)
-  #   - ck: integer, third node id (only for pulleys, else omitted or 0)
-  # ---------------------------------------------------------------
-  headers: [name, ci, cj, ck]
-  data:
-    # front lines
-    - [a6,1,25,33] #e.g. this is a pulley
-    - [A5,3,21]
-    - [A3,5,21]
-    - [A2,7,22]
-    - [A1,9,22]
-    - [A1,11,23]
-    - [A2,13,23]
-    - [A3,15,24]
-    - [A5,17,24]
-    - [a6,19,26,35]
-    - [AII,21,25]
-    - [AI,22,25]
-    - [AI,23,26]
-    - [AII,24,26]
-    - [amain,25,0]
-    - [amain,26,0]
-    # rear lines
-    - [a6,1,33,25]
-    - [br6,2,33,36]
-    - [br6,2,36,33]
-    - [br5,4,27]
-    - [br3,6,27]
-    - [br2,8,28]
-    - [br1,10,28]
-    - [br1,12,29]
-    - [br2,14,29]
-    - [br3,16,30]
-    - [br5,18,30]
-    - [a6,19,35,26]
-    - [br6,20,35,37]
-    - [br6,20,37,35]
-    - [BRII,27,31]
-    - [BRI,28,31]
-    - [BRI,29,32]
-    - [BRII,30,32]
-    - [BR-main-1,31,33]
-    - [BR-main-1,32,35]
-    - [M-line,33,36,34]
-    - [M-line,33,34,36]
-    - [M-line,35,34,37]
-    - [M-line,35,37,34]
-    - [Steering Tape,36,0]
-    - [Power Tape,34,0]
-    - [Steering Tape,37,0]
-
-
-
-
+    - [19, polars, {csv_file_path: "polars_CFD/19.csv"}]

data/TUDELFT_V3_KITE/vsm_settings.yaml

@@ -44,7 +44,7 @@ condition:
 # Define wing geometry files and discretization parameters
 wings:
     - name: V3_Kite                    # Wing identifier for output labeling
-      geometry_file: data/TUDELFT_V3_KITE/wing_geometry_polars_CFD.yaml
+      geometry_file: data/TUDELFT_V3_KITE/aero_geometry.yaml
       n_panels: 36                     # Total number of panels along wingspan
       n_groups: 1                      # Number of panel groups (must divide n_panels)
       spanwise_panel_distribution: LINEAR    # Panel spacing algorithm