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peterdsharpe
/
AeroSandbox
Aircraft design optimization made fast through modern automatic differentiation. Composable analysis tools for aerodynamics, propulsion, structures, trajectory design, and much more.
https://peterdsharpe.github.io/AeroSandbox/
MIT License
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Atmosphere model
#50
katherinezhao02
closed
3 years ago
1
NameError: name 'cas' is not defined
#49
StepLogic
closed
3 years ago
1
Fuselage with Rectangular Profile
#48
StepLogic
closed
3 years ago
2
Unsteady aero library
#47
peterdsharpe
closed
3 years ago
7
Bug fixes
#46
antoniosgeme
closed
3 years ago
1
Feat/airfoil viscous
#45
peterdsharpe
closed
3 years ago
0
Create FUNDING.yml
#44
peterdsharpe
closed
3 years ago
0
Hotfix/issue42 pytest
#43
Christophe-Foyer
closed
3 years ago
0
pytest is required but not included
#42
bismurphy
closed
3 years ago
3
Added `aerosandbox.numpy`
#41
peterdsharpe
closed
3 years ago
0
Update airplane.py
#40
Gilgahex
closed
3 years ago
1
Update requirements.txt
#39
Gilgahex
closed
3 years ago
1
Error running fitting example
#38
joyo44
closed
3 years ago
1
error when run the file" \examples\geometry_engine\airfoil\airfoil_xfoil_parallel.py"
#37
gkbatchelor
closed
3 years ago
4
No force output by panel1
#36
zjb19900907
closed
3 years ago
1
Airplane not considering Wing>xsecs>Airfoil: name or coordinates for draw()
#35
andresakle
closed
4 years ago
1
MAC calculation functions
#34
SzymonSzyszko
closed
4 years ago
0
MAC calculation function, c_ref = MAC and small bug fixed in example .py
#33
SzymonSzyszko
closed
4 years ago
1
Infeasible Problem Detected - CasLL1 alpha sweep with custom Cl, Cd and Cm functions
#32
alexandroslessis
closed
4 years ago
4
EXIT: Maximum Number of Iterations Exceeded.
#31
hen97
closed
4 years ago
3
Error Running casll1_fuselage_simple_analysis_point.py
#30
StepLogic
closed
4 years ago
2
Error Running vlm3_conventional.py
#29
StepLogic
closed
4 years ago
2
ployly module not found error.
#28
BradRR
closed
4 years ago
5
Continuous Integration
#27
KikeM
closed
4 years ago
1
Feature/versioneer
#26
KikeM
closed
4 years ago
1
ENH: removed xfoil as a mandatory dependency, cleaned-up requirements.txt
#25
KikeM
closed
4 years ago
0
Problems installing on a Mac
#24
KikeM
closed
4 years ago
3
Avoid comparing float to integer
#23
KikeM
closed
4 years ago
1
Set bounds to versions in setup.py
#22
KikeM
closed
4 years ago
1
Set CL instead of Alpha in OperatingPoint
#21
KikeM
closed
4 years ago
2
Include versioneer.py to have automatic version update in setup.py
#20
KikeM
closed
4 years ago
5
unit checking
#19
1ozturkbe
closed
4 years ago
1
Wing with a winglet
#18
KikeM
closed
4 years ago
15
Regarding Moments Estimation
#17
dnsuman25
closed
4 years ago
12
Issues with running the example code on Anaconda
#16
dnsuman25
closed
4 years ago
3
Numpy Error
#15
alexandroslessis
closed
4 years ago
3
Vlm4 fix
#14
peterdsharpe
closed
4 years ago
0
Vehicle firefly
#13
peterdsharpe
closed
4 years ago
0
Update README to reflect PyVista on conda-forge
#12
banesullivan
closed
4 years ago
0
Validation test
#11
jonititan
closed
4 years ago
3
Create vlm3_wild_turkey.py
#10
jonititan
closed
4 years ago
0
First few docstrings
#9
jonititan
closed
4 years ago
0
Question about fuselage
#8
ghost
closed
4 years ago
1
Keeping both a gui and a command line interface
#7
ghost
closed
4 years ago
1
Question about Moments vs Force and which to use for machines learning
#6
ghost
closed
4 years ago
3
Question about outputing airfoil/fuselage
#5
ghost
closed
4 years ago
4
Units
#4
jonititan
closed
4 years ago
5
Problem running the optimization example
#3
chiefenne
closed
4 years ago
3
VLM3 calculation prints out VLM2
#2
chiefenne
closed
4 years ago
1
s_ref assertion in geometry
#1
chiefenne
closed
4 years ago
1
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