Resolved minor typos for better readability#780
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jkirk5 merged 111 commits intoOpenMDAO:mainfrom Jun 5, 2025
Monstertov:fix-typos
Merged
Resolved minor typos for better readability#780jkirk5 merged 111 commits intoOpenMDAO:mainfrom Monstertov:fix-typos
jkirk5 merged 111 commits intoOpenMDAO:mainfrom
Monstertov:fix-typos
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jkirk5
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May 30, 2025
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Kenneth-T-Moore
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Jun 2, 2025
github-merge-queue
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removed this pull request from the merge queue due to failed status checks
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@jkirk5 Hi! I see it was removed from the merge queue. However i don't know what exactly fails. |
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Seems like an issue that is impacting several of our PRs at the moment, probably on our end. |
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Fixed a range of spelling mistakes in comments and text.
Details:
aviary/core/AviaryGroup.py, line 107:unneccesary→unnecessaryaviary/core/AviaryGroup.py, line 109:segements→segmentsaviary/core/PostMissionGroup.py, line 11:Congigure→Configureaviary/docs/developer_guide/unit_tests.md, line 65:acurate→accurateaviary/docs/developer_guide/unit_tests.md, line 76:usally→usuallyaviary/docs/getting_started/installation.md, line 167:avaliable→availableaviary/docs/misc_resources/comparison_to_flops.md, line 96:heterogenous→heterogeneousaviary/docs/misc_resources/glossary.md, line 45:homogenous→homogeneousaviary/docs/misc_resources/glossary.md, line 49:homogenous→homogeneousaviary/examples/external_subsystems/OAS_weight/OAS_wing_weight_analysis.py, line 179:intertia→inertiaaviary/examples/external_subsystems/OAS_weight/OAS_wing_weight_analysis.py, line 466:componenet→componentaviary/examples/external_subsystems/OAS_weight/OAS_wing_weight_analysis.py, line 497:funtion→functionaviary/examples/external_subsystems/simple_weight/simple_weight.py, line 3:horiztonal→horizontalaviary/examples/multi_mission/run_multimission_example_large_single_aisle.py, line 143:becuse→becauseaviary/interface/default_phase_info/height_energy_fiti.py, line 6:integeration→integrationaviary/interface/default_phase_info/height_energy_fiti.py, line 48:accomodate→accommodateaviary/interface/default_phase_info/two_dof.py, line 302:accomodate→accommodateaviary/interface/default_phase_info/two_dof_fiti.py, line 14:integeration→integrationaviary/interface/default_phase_info/two_dof_fiti.py, line 159:accomodate→accommodateaviary/interface/default_phase_info/two_dof_fiti_deprecated.py, line 14:integeration→integrationaviary/interface/reports.py, line 75:containts→containsaviary/interface/test/test_cmd_entry_points.py, line 15:seperately→separatelyaviary/interface/test/test_height_energy_mission.py, line 151:seperately→separatelyaviary/interface/test/test_reserve_support.py, line 14:innacurate→inaccurateaviary/interface/test_installation.py, line 89:avaliable→availableaviary/interface/utils/markdown_utils.py, line 52:avaliable→availableaviary/interface/utils/markdown_utils.py, line 96:paretheses→parenthesesaviary/mission/flops_based/ode/landing_ode.py, line 48:signficant→significantaviary/mission/gasp_based/ode/constraints/flight_constraints.py, line 141:accross→acrossaviary/mission/gasp_based/ode/time_integration_base_classes.py, line 341:paramaters→parametersaviary/mission/height_energy_problem_configurator.py, line 215:intitial→initialaviary/mission/solved_two_dof_problem_configurator.py, line 143:intitial→initialaviary/mission/two_dof_problem_configurator.py, line 365:intitial→initialaviary/mission/two_dof_problem_configurator.py, line 467:continous→continuousaviary/subsystems/aerodynamics/flops_based/drag.py, line 11:coefficent→coefficientaviary/subsystems/aerodynamics/flops_based/drag.py, line 146:contirbutions→contributionsaviary/subsystems/aerodynamics/flops_based/drag.py, line 150:cummulative→cumulativeaviary/subsystems/aerodynamics/flops_based/ground_effect.py, line 20:accomodate→accommodateaviary/subsystems/aerodynamics/gasp_based/test/test_gaspaero.py, line 207:overriden→overriddenaviary/subsystems/aerodynamics/gasp_based/test/test_solved_aero_group.py, line 137:addreses→addressesaviary/subsystems/aerodynamics/test/test_gasp_drag.py, line 16:addreses→addressesaviary/subsystems/geometry/flops_based/wetted_area_total.py, line 10:enought→enoughaviary/subsystems/geometry/gasp_based/fuselage.py, line 74:noticable→noticeableaviary/subsystems/geometry/gasp_based/test/test_wing.py, line 539:dimentional→dimensionalaviary/subsystems/mass/flops_based/electrical.py, line 83:susbsystems→subsystemsaviary/subsystems/mass/flops_based/engine_pod.py, line 72:discrepency→discrepancyaviary/subsystems/mass/flops_based/landing_gear.py, line 308:configuation→configurationaviary/subsystems/mass/gasp_based/equipment_and_useful_load.py, line 858:calulated→calculatedaviary/subsystems/mass/gasp_based/equipment_and_useful_load.py, line 869:calulated→calculatedaviary/subsystems/mass/gasp_based/fixed.py, line 621:avaliable→availableaviary/subsystems/mass/gasp_based/fixed.py, line 2712:noticable→noticeableaviary/subsystems/mass/gasp_based/test/test_fixed.py, line 533:arbitarary→arbitraryaviary/subsystems/mass/gasp_based/test/test_fuel.py, line 58:calulated→calculatedaviary/subsystems/mass/gasp_based/test/test_fuel.py, line 61:calulated→calculatedaviary/subsystems/mass/gasp_based/test/test_fuel.py, line 64:calulated→calculatedaviary/subsystems/mass/gasp_based/test/test_fuel.py, line 206:calulated→calculatedaviary/subsystems/mass/gasp_based/test/test_fuel.py, line 209:calulated→calculatedaviary/subsystems/mass/gasp_based/test/test_fuel.py, line 212:calulated→calculatedaviary/subsystems/mass/gasp_based/test/test_fuel.py, line 713:calulated→calculatedaviary/subsystems/mass/gasp_based/test/test_fuel.py, line 716:calulated→calculatedaviary/subsystems/mass/gasp_based/test/test_fuel.py, line 719:calulated→calculatedaviary/subsystems/propulsion/engine_deck.py, line 302:avaliable→availableaviary/subsystems/propulsion/engine_deck.py, line 440:variabes→variablesaviary/subsystems/propulsion/engine_deck.py, line 463:calulated→calculatedaviary/subsystems/propulsion/engine_deck.py, line 481:convertable→convertibleaviary/subsystems/propulsion/engine_deck.py, line 509:convertable→convertibleaviary/subsystems/propulsion/engine_deck.py, line 534:avaliable→availableaviary/subsystems/propulsion/engine_deck.py, line 839:potentialy→potentiallyaviary/subsystems/propulsion/engine_deck.py, line 921:avaliable→availableaviary/subsystems/propulsion/engine_deck.py, line 928:avaliable→availableaviary/subsystems/propulsion/engine_deck.py, line 1174:paretheses→parenthesesaviary/subsystems/propulsion/propeller/hamilton_standard.py, line 15:seperate→separateaviary/subsystems/propulsion/propeller/hamilton_standard.py, line 61:coefficeints→coefficientsaviary/subsystems/propulsion/propeller/hamilton_standard.py, line 230:coeffient→coefficientaviary/subsystems/propulsion/propeller/propeller_performance.py, line 109:derivitive→derivativeaviary/subsystems/propulsion/propeller/propeller_performance.py, line 627:infomation→informationaviary/subsystems/propulsion/propeller/test/test_propeller_performance.py, line 22:derivitives→derivativesaviary/subsystems/propulsion/propulsion_builder.py, line 34:reccomended→recommendedaviary/subsystems/propulsion/utils.py, line 127:avaliable→availableaviary/subsystems/propulsion/utils.py, line 236:avaliable→availableaviary/subsystems/test/subsystem_tester.py, line 21:subsytem→subsystemaviary/subsystems/test/test_premission.py, line 121:inital→initialaviary/subsystems/test/test_premission.py, line 212:overriden→overriddenaviary/subsystems/test/test_premission.py, line 312:overriden→overriddenaviary/utils/csv_data_file.py, line 72:avaliable→availableaviary/utils/data_interpolator_builder.py, line 29:executuion→executionaviary/utils/data_interpolator_builder.py, line 119:strucured→structuredaviary/utils/data_interpolator_builder.py, line 140:guarenteed→guaranteedaviary/utils/develop_metadata.py, line 56:nameing→namingaviary/utils/develop_metadata.py, line 174:nameing→namingaviary/utils/doctape.py, line 21:execption→exceptionaviary/utils/engine_deck_conversion.py, line 374:varaiables→variablesaviary/utils/functions.py, line 90:varibles→variablesaviary/utils/merge_hierarchies.py, line 131:hierarhcy→hierarchyaviary/utils/preprocessors.py, line 137:exmaple→exampleaviary/utils/preprocessors.py, line 339:compatability→compatibilityaviary/utils/preprocessors.py, line 347:mantain→maintainaviary/utils/propeller_map_conversion.py, line 83:varaiables→variablesaviary/utils/test/test_csv_data_file.py, line 91:temperary→temporaryaviary/utils/test/test_csv_data_file.py, line 103:temperary→temporaryaviary/variable_info/enums.py, line 80:Currenly→Currentlyaviary/variable_info/functions.py, line 134:speficying→specifyingaviary/variable_info/functions.py, line 349:overriden→overriddenaviary/variable_info/functions.py, line 511:quanitity→quantityaviary/variable_info/variable_meta_data.py, line 1324:Auxilary→Auxiliaryaviary/variable_info/variable_meta_data.py, line 3385:coefficent→coefficientaviary/variable_info/variable_meta_data.py, line 3474:millitary→militaryaviary/variable_info/variable_meta_data.py, line 4444:diamter→diameteraviary/variable_info/variable_meta_data.py, line 7633:beginnning→beginningaviary/visualization/aircraft_3d_model.py, line 225:hierachy→hierarchyOnly documentation-style text was changed.