Merge pull request #976 from xjjiang/BWB_FLOPS_Docs

FLOPS based BWB implementation documentation

Author: jkirk5

aviary/docs/_toc.yml

@@ -54,7 +54,8 @@ parts:
       - file: user_guide/multi_mission
       - file: user_guide/off_design_missions
       - file: user_guide/payload_range_functionality
-      - file: user_guide/features/blended_wing_body
+      - file: user_guide/features/blended_wing_body_GASP
+      - file: user_guide/features/blended_wing_body_FLOPS
     - file: user_guide/troubleshooting
 
 - caption: Examples

aviary/docs/theory_guide/gasp_based_bwb.ipynb

@@ -48,7 +48,7 @@
    "source": [
     "# GASP based BWB model implementation\n",
     "\n",
-    "Modeling of GASP based blended wing body (BWB) aircraft is similar to that of the conventional aircraft but with several key differences. This page is a record of the development. For users, please read [Blended Wing Body Modeling](../user_guide/features/blended_wing_body) in the user guide.\n",
+    "Modeling of GASP based blended wing body (BWB) aircraft is similar to that of the conventional aircraft but with several key differences. This page is a record of the development. For users, please read [Blended Wing Body Modeling](../user_guide/features/blended_wing_body_GASP) in the user guide.\n",
     "\n",
     "## BWB geometry subsystem\n",
     "\n",
@@ -456,7 +456,7 @@
  ],
  "metadata": {
   "kernelspec": {
-   "display_name": "Python 3 (ipykernel)",
+   "display_name": "base",
    "language": "python",
    "name": "python3"
   },
@@ -470,7 +470,7 @@
    "name": "python",
    "nbconvert_exporter": "python",
    "pygments_lexer": "ipython3",
-   "version": "3.12.3"
+   "version": "3.12.9"
   }
  },
  "nbformat": 4,

aviary/docs/user_guide/features/blended_wing_body_FLOPS.ipynb

@@ -19,7 +19,7 @@
    "id": "267d6a8d",
    "metadata": {},
    "source": [
-    "# Blended Wing Body Modeling\n",
+    "# GASP Based Blended Wing Body Modeling\n",
     "\n",
     "The blended wing body aircraft is modeled following GASP implementation. It is important to point out the the Aviary implementation is limited to certain assumptions. To model a special model, the user must read this document carefully to see it is within the scope of the Aviary implementation.\n",
     "\n",

…r_guide/features/blended_wing_body.ipynb …de/features/blended_wing_body_GASP.ipynbaviary/docs/user_guide/features/blended_wing_body.ipynb renamed to aviary/docs/user_guide/features/blended_wing_body_GASP.ipynb aviary/docs/user_guide/features/blended_wing_body.ipynb renamed to aviary/docs/user_guide/features/blended_wing_body_GASP.ipynb

@@ -394,7 +394,11 @@ def add_post_mission_systems(self, aviary_group):
             )
 
         if aviary_group.post_mission_info['include_landing']:
-            self._add_landing_systems(aviary_group)
+            if 'aircraft:wing:area' in aviary_group.aviary_inputs:
+                self._add_landing_systems(aviary_group)
+            else:
+                print('Aircraft.Wing.AREA is not given. Set include_landing = False')
+                aviary_group.post_mission_info['include_landing'] = False
 
         aviary_group.add_subsystem(
             'range_constraint',

aviary/docs/user_guide/images/BWB_FLOPS_Fuselage_Simple_Geom.png

@@ -164,6 +164,7 @@ mission:summary:fuel_flow_scaler,1.0,unitless
 settings:aerodynamics_method,FLOPS,unitless
 settings:equations_of_motion,height_energy,unitless
 settings:mass_method,FLOPS,unitless
+settings:verbosity,1,unitless
 
 # Unconverted Values
 AERIN.FLLDG,11000