Bump version and doc fixes (#465)

sabakhshi · web-flow · commit e645a31d8362 · 2025-06-27T07:19:41.000+09:00
diff --git a/openaerostruct/__init__.py b/openaerostruct/__init__.py
@@ -1 +1 @@
-__version__ = "2.10.1"
+__version__ = "2.11.0"
diff --git a/openaerostruct/docs/index.rst b/openaerostruct/docs/index.rst
@@ -76,7 +76,7 @@ Source Docs
 Please Cite Us!
 ---------------
 
-If you use OpenAeroStruct, please cite the `following paper <https://www.researchgate.net/publication/322991521_Open-source_coupled_aerostructural_optimization_using_Python>__`:
+If you use OpenAeroStruct, please cite the `following paper <https://www.researchgate.net/publication/322991521_Open-source_coupled_aerostructural_optimization_using_Python>`_:
 
 John P. Jasa, John T. Hwang, and Joaquim R. R. A. Martins. "Open-source coupled aerostructural optimization using Python." Structural and Multidisciplinary Optimization 57.4 (2018): 1815-1827. DOI: 10.1007/s00158-018-1912-8
 
@@ -96,7 +96,7 @@ John P. Jasa, John T. Hwang, and Joaquim R. R. A. Martins. "Open-source coupled
    }
 
 
-If you use the wingbox structural model, fuel-weight inertial loads, or structural-weight inertial loads, please also cite the `following paper <https://www.researchgate.net/publication/327654423_Low-Fidelity_Aerostructural_Optimization_of_Aircraft_Wings_with_a_Simplified_Wingbox_Model_Using_OpenAeroStruct>__`:
+If you use the wingbox structural model, fuel-weight inertial loads, or structural-weight inertial loads, please also cite the `following paper <https://www.researchgate.net/publication/327654423_Low-Fidelity_Aerostructural_Optimization_of_Aircraft_Wings_with_a_Simplified_Wingbox_Model_Using_OpenAeroStruct>`_:
 
 Shamsheer S. Chauhan and Joaquim R. R. A. Martins, “Low-Fidelity Aerostructural Optimization of Aircraft Wings with a Simplified Wingbox Model Using OpenAeroStruct,” Proceedings of the 6th International Conference on Engineering Optimization, EngOpt 2018, Springer, Lisbon, Portugal, September 2018, pp. 418–431. doi:10.1007/978-3-319-97773-7 38
 
@@ -114,7 +114,7 @@ Shamsheer S. Chauhan and Joaquim R. R. A. Martins, “Low-Fidelity Aerostructura
    }
 
 
-If using point-mass loads or thrust loads, please cite the following `paper (https://www.researchgate.net/publication/333806174_How_Certain_Physical_Considerations_Impact_Aerostructural_Wing_Optimization)__`.
+If using point-mass loads or thrust loads, please cite the following `paper (https://www.researchgate.net/publication/333806174_How_Certain_Physical_Considerations_Impact_Aerostructural_Wing_Optimization)`_.
 
 John P. Jasa, Shamsheer S. Chauhan, Justin S. Gray, and Joaquim R. R. A. Martins, “How Certain Physical Considerations Impact Aerostructural Wing Optimization,” AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Dallas, TX, 2019. doi:10.2514/6.2019-3242
 
diff --git a/openaerostruct/geometry/ffd_component.py b/openaerostruct/geometry/ffd_component.py
@@ -1,4 +1,4 @@
-""" Manipulate geometry mesh based on high-level design parameters. """
+"""Manipulate geometry mesh based on high-level design parameters."""
 
 import numpy as np
 

Original file line number	Diff line number	Diff line change
`@@ -1 +1 @@`
`1`		`-__version__ = "2.10.1"`
	`1`	`+__version__ = "2.11.0"`
Original file line number	Diff line number	Diff line change
`@@ -76,7 +76,7 @@ Source Docs`
`76`	`76`	`Please Cite Us!`
`77`	`77`	`---------------`
`78`	`78`
`79`		-If you use OpenAeroStruct, please cite the `following paper <https://www.researchgate.net/publication/322991521_Open-source_coupled_aerostructural_optimization_using_Python>__`:
	`79`	+If you use OpenAeroStruct, please cite the `following paper <https://www.researchgate.net/publication/322991521_Open-source_coupled_aerostructural_optimization_using_Python>`_:
`80`	`80`
`81`	`81`	`John P. Jasa, John T. Hwang, and Joaquim R. R. A. Martins. "Open-source coupled aerostructural optimization using Python." Structural and Multidisciplinary Optimization 57.4 (2018): 1815-1827. DOI: 10.1007/s00158-018-1912-8`
`82`	`82`
`@@ -96,7 +96,7 @@ John P. Jasa, John T. Hwang, and Joaquim R. R. A. Martins. "Open-source coupled`
`96`	`96`	`}`
`97`	`97`
`98`	`98`
`99`		-If you use the wingbox structural model, fuel-weight inertial loads, or structural-weight inertial loads, please also cite the `following paper <https://www.researchgate.net/publication/327654423_Low-Fidelity_Aerostructural_Optimization_of_Aircraft_Wings_with_a_Simplified_Wingbox_Model_Using_OpenAeroStruct>__`:
	`99`	+If you use the wingbox structural model, fuel-weight inertial loads, or structural-weight inertial loads, please also cite the `following paper <https://www.researchgate.net/publication/327654423_Low-Fidelity_Aerostructural_Optimization_of_Aircraft_Wings_with_a_Simplified_Wingbox_Model_Using_OpenAeroStruct>`_:
`100`	`100`
`101`	`101`	`Shamsheer S. Chauhan and Joaquim R. R. A. Martins, “Low-Fidelity Aerostructural Optimization of Aircraft Wings with a Simplified Wingbox Model Using OpenAeroStruct,” Proceedings of the 6th International Conference on Engineering Optimization, EngOpt 2018, Springer, Lisbon, Portugal, September 2018, pp. 418–431. doi:10.1007/978-3-319-97773-7 38`
`102`	`102`
`@@ -114,7 +114,7 @@ Shamsheer S. Chauhan and Joaquim R. R. A. Martins, “Low-Fidelity Aerostructura`
`114`	`114`	`}`
`115`	`115`
`116`	`116`
`117`		-If using point-mass loads or thrust loads, please cite the following `paper (https://www.researchgate.net/publication/333806174_How_Certain_Physical_Considerations_Impact_Aerostructural_Wing_Optimization)__`.
	`117`	+If using point-mass loads or thrust loads, please cite the following `paper (https://www.researchgate.net/publication/333806174_How_Certain_Physical_Considerations_Impact_Aerostructural_Wing_Optimization)`_.
`118`	`118`
`119`	`119`	`John P. Jasa, Shamsheer S. Chauhan, Justin S. Gray, and Joaquim R. R. A. Martins, “How Certain Physical Considerations Impact Aerostructural Wing Optimization,” AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Dallas, TX, 2019. doi:10.2514/6.2019-3242`
`120`	`120`
Original file line number	Diff line number	Diff line change
`@@ -1,4 +1,4 @@`
`1`		`-""" Manipulate geometry mesh based on high-level design parameters. """`
	`1`	`+"""Manipulate geometry mesh based on high-level design parameters."""`
`2`	`2`
`3`	`3`	`import numpy as np`
`4`	`4`