Ecosyste.ms: Issues
An open API service for providing issue and pull request metadata for open source projects.
GitHub / peterdsharpe/AeroSandbox issues and pull requests
#138 - Fix invalid escape sequence in math docstring
Pull Request -
State: closed - Opened by fgrbr 5 months ago
- 1 comment
#134 - Control surface deflection is not working in the analysis
Issue -
State: open - Opened by JurajCe 8 months ago
- 2 comments
#133 - Feature: Include a `xsec_centroid` function for the WingXSec class (code provided)
Issue -
State: open - Opened by carsonwmoon 8 months ago
- 2 comments
#132 - Issue with np.diff()
Issue -
State: closed - Opened by joyo44 8 months ago
- 2 comments
#131 - Airfoil control surface / hinged geometry not smooth
Issue -
State: closed - Opened by benberry3d 8 months ago
- 2 comments
#130 - _DynamicsPointMassBaseClass.__getitem__(self, index: int) doesn't work for slices like in tutorial "06 - 3D Aircraft Dynamics for Engine-Out Analysis.ipynb"
Issue -
State: closed - Opened by carsonwmoon 8 months ago
- 1 comment
#129 - Fresh install of pip install aerosandbox[full,test], and it fails one test
Issue -
State: closed - Opened by carsonwmoon 8 months ago
- 1 comment
#128 - aerosandbox.geometry.wing.control_surface_area does not work
Issue -
State: closed - Opened by Daniel-E-B 8 months ago
- 2 comments
#127 - LEM on Kulfan airfoils
Issue -
State: closed - Opened by guillaume-florent 8 months ago
- 2 comments
#119 - Any list of the numpy supported functions?
Issue -
State: closed - Opened by mrrezaie 10 months ago
- 7 comments
#117 - Example usage of "linear C_L model"
Issue -
State: closed - Opened by pareal 10 months ago
- 2 comments
#116 - Compatibility with python 3.12
Issue -
State: closed - Opened by leomariga 11 months ago
- 2 comments
#113 - NumPy 1.25+ breaks something with NeuralFoil Optimization
Issue -
State: closed - Opened by peterdsharpe 12 months ago
- 1 comment
#103 - Update tutorial 06
Issue -
State: closed - Opened by mcleantom over 1 year ago
- 1 comment
#101 - is Opti() not supported for optimization of CST parameters of airfoils
Issue -
State: closed - Opened by Zcaic over 1 year ago
- 11 comments
#99 - don't use generate_polar_function before AeroBuildup.run()
Issue -
State: closed - Opened by Zcaic over 1 year ago
- 5 comments
#98 - There seems to be a problem with the display of symmetrical wings with dihedral
Issue -
State: closed - Opened by Zcaic over 1 year ago
- 4 comments
#97 - Fixed np.interp for symbolic xp and fp
Pull Request -
State: closed - Opened by carlitador over 1 year ago
- 1 comment
#95 - rename: Remove all spaces from filenames and replace with underscores
Pull Request -
State: closed - Opened by ThomasGreenhill over 1 year ago
- 2 comments
#94 - airfoil.generate_polars can't work well in Ubuntu
Issue -
State: closed - Opened by Zcaic over 1 year ago
- 12 comments
#93 - Correcting Torenbeek
Pull Request -
State: closed - Opened by Dirkjoost over 1 year ago
- 3 comments
#92 - Last updates NL LL
Pull Request -
State: closed - Opened by Yashil99 over 1 year ago
#91 - Nonlinear Lifting Line code from Yashil + Validation and other Improvements
Pull Request -
State: closed - Opened by peterdsharpe over 1 year ago
#89 - Inconsistent rotation convention in operating_point
Issue -
State: closed - Opened by carlitador over 1 year ago
- 3 comments
#87 - Fuselage Display
Issue -
State: closed - Opened by VallesMarinerisExplorer almost 2 years ago
- 1 comment
#86 - ControlSurface not working
Issue -
State: closed - Opened by max-97 almost 2 years ago
#84 - Question: STL Support?
Issue -
State: closed - Opened by PowerBroker2 about 2 years ago
#83 - 3D Panel method
Issue -
State: closed - Opened by enricostragiotti about 2 years ago
- 1 comment
#82 - asb.Opti() as a Singleton
Pull Request -
State: closed - Opened by syker-uk about 2 years ago
#81 - VLM for trajectory optimization
Issue -
State: open - Opened by cdhainaut about 2 years ago
- 3 comments
#80 - How to draw Cp distribution on 3D wing?
Issue -
State: closed - Opened by HYB777 about 2 years ago
- 2 comments
#77 - Tutorial 01 - Vortex Lattice Method is not working
Issue -
State: closed - Opened by jannav84 over 2 years ago
- 3 comments
#75 - Help
Issue -
State: closed - Opened by Arthur19950212 over 2 years ago
- 1 comment
#74 - Add coordinates for the generic airfoils
Pull Request -
State: closed - Opened by msberk almost 3 years ago
- 1 comment
#73 - Importing aerosandbox.library.airfoils raises warnings
Issue -
State: closed - Opened by msberk almost 3 years ago
- 1 comment
#72 - 4h installing and it keeps going
Issue -
State: closed - Opened by dgo2001 almost 3 years ago
- 2 comments
#71 - AVL Fortran runtime error: End of file
Issue -
State: closed - Opened by sr71684 almost 3 years ago
- 8 comments
#70 - Add new features to `AVL`; Add new syntax for analysis-specific options in geometry stack
Pull Request -
State: closed - Opened by peterdsharpe almost 3 years ago
- 5 comments
#69 - Merging `annick-fixes` into `develop`
Pull Request -
State: closed - Opened by peterdsharpe almost 3 years ago
#68 - object has no attribute 'front_left_vertices'
Issue -
State: closed - Opened by carlitador about 3 years ago
#67 - AeroSandbox use for aero/hydrostructural model
Issue -
State: closed - Opened by carlitador about 3 years ago
#66 - Wrong requirements when installing via pip
Issue -
State: closed - Opened by hughjward about 3 years ago
- 3 comments
#60 - Openvsp geometry conversion to Aerosandbox
Pull Request -
State: open - Opened by opme over 3 years ago
#59 - added plt.show()
Pull Request -
State: closed - Opened by chiefenne over 3 years ago
- 1 comment
#58 - add docker/jupyter
Pull Request -
State: open - Opened by scivm over 3 years ago
- 2 comments
#57 - Use multivariate regression analysis to obtain "Application Laws" for Airfoil Polar Data
Issue -
State: closed - Opened by Dirk07 over 3 years ago
- 1 comment
#56 - Add Explanation and Conventions on Wing Modelling Method(s)
Issue -
State: closed - Opened by Dirk07 over 3 years ago
- 1 comment
#55 - Add columns for hinge force coefficients (c.Fx, cFy) in XFoil's Airfoil Polar File
Issue -
State: closed - Opened by Dirk07 over 3 years ago
- 1 comment
#54 - Incorrect Inviscid Airfoil Analysis
Issue -
State: closed - Opened by GodotMisogi over 3 years ago
- 4 comments
#52 - Unable to Run Example Script
Issue -
State: closed - Opened by KarlTaht over 3 years ago
- 7 comments
#51 - Feature/unsteady
Pull Request -
State: closed - Opened by antoniosgeme over 3 years ago
- 2 comments
#50 - Atmosphere model
Pull Request -
State: closed - Opened by katherinezhao02 over 3 years ago
- 1 comment
#49 - NameError: name 'cas' is not defined
Issue -
State: closed - Opened by StepLogic over 3 years ago
- 1 comment
#48 - Fuselage with Rectangular Profile
Issue -
State: closed - Opened by StepLogic over 3 years ago
- 2 comments
#47 - Unsteady aero library
Pull Request -
State: closed - Opened by peterdsharpe over 3 years ago
- 7 comments
#46 - Bug fixes
Pull Request -
State: closed - Opened by antoniosgeme over 3 years ago
- 1 comment
#45 - Feat/airfoil viscous
Pull Request -
State: closed - Opened by peterdsharpe over 3 years ago
#44 - Create FUNDING.yml
Pull Request -
State: closed - Opened by peterdsharpe almost 4 years ago
#43 - Hotfix/issue42 pytest
Pull Request -
State: closed - Opened by Christophe-Foyer almost 4 years ago
#42 - pytest is required but not included
Issue -
State: closed - Opened by bismurphy almost 4 years ago
- 3 comments
#41 - Added `aerosandbox.numpy`
Pull Request -
State: closed - Opened by peterdsharpe almost 4 years ago
#40 - Update airplane.py
Pull Request -
State: closed - Opened by Gilgahex almost 4 years ago
- 1 comment
#39 - Update requirements.txt
Pull Request -
State: closed - Opened by Gilgahex almost 4 years ago
- 1 comment
#38 - Error running fitting example
Issue -
State: closed - Opened by joyo44 almost 4 years ago
- 1 comment
#37 - error when run the file" \examples\geometry_engine\airfoil\airfoil_xfoil_parallel.py"
Issue -
State: closed - Opened by gkbatchelor about 4 years ago
- 4 comments
#36 - No force output by panel1
Issue -
State: closed - Opened by zjb19900907 about 4 years ago
- 1 comment
#35 - Airplane not considering Wing>xsecs>Airfoil: name or coordinates for draw()
Issue -
State: closed - Opened by andresakle over 4 years ago
- 1 comment
#34 - MAC calculation functions
Pull Request -
State: closed - Opened by SzymonSzyszko over 4 years ago
#33 - MAC calculation function, c_ref = MAC and small bug fixed in example .py
Pull Request -
State: closed - Opened by SzymonSzyszko over 4 years ago
- 1 comment
#32 - Infeasible Problem Detected - CasLL1 alpha sweep with custom Cl, Cd and Cm functions
Issue -
State: closed - Opened by alexandroslessis over 4 years ago
- 4 comments
#31 - EXIT: Maximum Number of Iterations Exceeded.
Issue -
State: closed - Opened by hen97 over 4 years ago
- 3 comments
#30 - Error Running casll1_fuselage_simple_analysis_point.py
Issue -
State: closed - Opened by StepLogic over 4 years ago
- 2 comments
#29 - Error Running vlm3_conventional.py
Issue -
State: closed - Opened by StepLogic over 4 years ago
- 2 comments
#28 - ployly module not found error.
Issue -
State: closed - Opened by BradRR over 4 years ago
- 5 comments
#27 - Continuous Integration
Issue -
State: closed - Opened by KikeM over 4 years ago
- 1 comment
#26 - Feature/versioneer
Pull Request -
State: closed - Opened by KikeM over 4 years ago
- 1 comment
#25 - ENH: removed xfoil as a mandatory dependency, cleaned-up requirements.txt
Pull Request -
State: closed - Opened by KikeM over 4 years ago
#24 - Problems installing on a Mac
Issue -
State: closed - Opened by KikeM over 4 years ago
- 3 comments
#23 - Avoid comparing float to integer
Issue -
State: closed - Opened by KikeM over 4 years ago
- 1 comment
#22 - Set bounds to versions in setup.py
Issue -
State: closed - Opened by KikeM over 4 years ago
- 1 comment
#21 - Set CL instead of Alpha in OperatingPoint
Issue -
State: closed - Opened by KikeM over 4 years ago
- 2 comments
#20 - Include versioneer.py to have automatic version update in setup.py
Issue -
State: closed - Opened by KikeM over 4 years ago
- 5 comments
#19 - unit checking
Issue -
State: closed - Opened by 1ozturkbe over 4 years ago
- 1 comment
#18 - Wing with a winglet
Issue -
State: closed - Opened by KikeM over 4 years ago
- 15 comments
#17 - Regarding Moments Estimation
Issue -
State: closed - Opened by dnsuman25 almost 5 years ago
- 12 comments
#16 - Issues with running the example code on Anaconda
Issue -
State: closed - Opened by dnsuman25 almost 5 years ago
- 3 comments
#15 - Numpy Error
Issue -
State: closed - Opened by alexandroslessis almost 5 years ago
- 3 comments
#14 - Vlm4 fix
Pull Request -
State: closed - Opened by peterdsharpe almost 5 years ago
#13 - Vehicle firefly
Pull Request -
State: closed - Opened by peterdsharpe about 5 years ago
#12 - Update README to reflect PyVista on conda-forge
Pull Request -
State: closed - Opened by banesullivan about 5 years ago
#11 - Validation test
Issue -
State: closed - Opened by jonititan over 5 years ago
- 3 comments
#10 - Create vlm3_wild_turkey.py
Pull Request -
State: closed - Opened by jonititan over 5 years ago
#9 - First few docstrings
Pull Request -
State: closed - Opened by jonititan over 5 years ago
#8 - Question about fuselage
Issue -
State: closed - Opened by ghost over 5 years ago
- 1 comment
#7 - Keeping both a gui and a command line interface
Issue -
State: closed - Opened by ghost over 5 years ago
- 1 comment
#6 - Question about Moments vs Force and which to use for machines learning
Issue -
State: closed - Opened by ghost over 5 years ago
- 3 comments
#5 - Question about outputing airfoil/fuselage
Issue -
State: closed - Opened by ghost over 5 years ago
- 4 comments
#4 - Units
Issue -
State: closed - Opened by jonititan over 5 years ago
- 5 comments
#3 - Problem running the optimization example
Issue -
State: closed - Opened by chiefenne over 5 years ago
- 3 comments
#2 - VLM3 calculation prints out VLM2
Issue -
State: closed - Opened by chiefenne over 5 years ago
- 1 comment