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abdbeam-0.2.1
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مشاهده بیشتر
تبلیغات ما
مشتریان به طور فزاینده ای آنلاین هستند. تبلیغات می تواند به آنها کمک کند تا کسب و کار شما را پیدا کنند.
مشاهده بیشتر
تبلیغات ما
مشتریان به طور فزاینده ای آنلاین هستند. تبلیغات می تواند به آنها کمک کند تا کسب و کار شما را پیدا کنند.
مشاهده بیشترتوضیحات
Cross section analysis of composite material beams of any shape.
| ویژگی | مقدار |
|---|---|
| سیستم عامل | - |
| نام فایل | abdbeam-0.2.1 |
| نام | abdbeam |
| نسخه کتابخانه | 0.2.1 |
| نگهدارنده | [] |
| ایمیل نگهدارنده | [] |
| نویسنده | Danilo S. Victorazzo |
| ایمیل نویسنده | victorazzo@gmail.com |
| آدرس صفحه اصلی | https://github.com/victorazzo/abdbeam |
| آدرس اینترنتی | https://pypi.org/project/abdbeam/ |
| مجوز | BSD-3 |
# Abdbeam : composites cross section analysis
A Python package for the cross section analysis of composite material beams of any shape.
## Main features
These are a few things you can do with **Abdbeam**:
* Use a fast thin-walled anisotropic composite beam theory including closed cells, open branches, shear connectors and booms (discrete stiffeners containing axial and torsional stiffnesses);
* Recover replacement stiffnesses (EA, EIyy, EIzz, EIyz, GJ) and/or a full 4 x 4 stiffness matrix for beams with arbitrary layups and shapes;
* Recover centroid and shear center locations;
* Obtain internal load distributions (Nx, Nxy, Mx, My, Mxy for segments; Px and Tx for booms) for a large number of cross section load cases (defined by Px, My, Mz, Tz, Vy and Vz section loads);
* Plot cross sections, their properties and internal loads.
## Installing
Install using PyPI ([Python package index](https://pypi.org/project/abdbeam)) :
```sh
pip install abdbeam
```
## Source and Documentation
The source code is hosted on GitHub at https://github.com/victorazzo/abdbeam and the documentation can be found at https://docs.abdbeam.org.
## Dependencies
- [NumPy](https://www.numpy.org)
- [Pandas](https://pandas.pydata.org)
- [Matplotlib](https://matplotlib.org)
## Example
Let's use **Abdbeam** to analyze the cross section with two closed cells below:
<img src="https://user-images.githubusercontent.com/24232637/50049830-266c6380-00bc-11e9-808d-97896d3f3e16.png" width="400">
Start creating the section materials, its points and segments (we'll also calculate the section properties and request a summary at the end):
```python
import abdbeam as ab
sc = ab.Section()
# Create a materials dictionary:
mts = dict()
mts[1] = ab.Laminate()
ply_mat = ab.PlyMaterial(0.166666, 148000, 9650, 4550, 0.3)
mts[1].ply_materials[1] = ply_mat
mts[1].plies = [[0,1]]*6 + [[45,1]]*6
# Create a points dictionary based on Y and Z point coordinates:
pts = dict()
pts[1] = ab.Point(0, -35)
pts[2] = ab.Point(-50, -35)
pts[3] = ab.Point(-50, 35)
pts[4] = ab.Point(0, 35)
pts[5] = ab.Point(50, 35)
pts[6] = ab.Point(50, -35)
# Create a segments dictionary referencing point and material ids:
sgs = dict()
sgs[1] = ab.Segment(1,2,1)
sgs[2] = ab.Segment(2,3,1)
sgs[3] = ab.Segment(3,4,1)
sgs[4] = ab.Segment(4,1,1)
sgs[5] = ab.Segment(4,5,1)
sgs[6] = ab.Segment(5,6,1)
sgs[7] = ab.Segment(6,1,1)
# Point the dictionaries to the section
sc.materials = mts
sc.points = pts
sc.segments = sgs
# Calculate and output section properties
sc.calculate_properties()
sc.summary()
```
Which prints:
```sh
Section Summary
===============
Number of points: 6
Number of segments: 7
Number of cells: 2
Centroid
--------
yc = -2.67780636e-01
zc = 0.00000000e+00
Shear Center
------------
ys = 2.35301214e-03
zs = -1.45758049e-03
Replacement Stiffnesses
-----------------------
EA = 6.80329523e+07
EIyy = 5.24834340e+10
EIzz = 8.36408748e+10
EIyz = 0.00000000e+00
GJ = 1.23762317e+10
EImax = 8.36408748e+10
EImin = 5.24834340e+10
Angle = 0.00000000e+00
[P_c] - Beam Stiffness Matrix at the Centroid
---------------------------------------------
[[ 6.80329523e+07 0.00000000e+00 2.46320132e+05 -1.43701515e+08]
[ 0.00000000e+00 5.24834340e+10 0.00000000e+00 0.00000000e+00]
[ 2.46320132e+05 0.00000000e+00 8.36408748e+10 -2.12142163e+07]
[-1.43701515e+08 0.00000000e+00 -2.12142163e+07 1.23762317e+10]]
[W_c] - Beam Compliance Matrix at the Centroid
----------------------------------------------
[[1.50683149e-08 0.00000000e+00 1.66286490e-28 1.74959530e-10]
[0.00000000e+00 1.90536313e-11 0.00000000e+00 0.00000000e+00]
[1.57282135e-25 0.00000000e+00 1.19558821e-11 2.04936911e-14]
[1.74959530e-10 0.00000000e+00 2.04936911e-14 8.28315446e-11]]
[P] - Beam Stiffness Matrix at the Origin
-----------------------------------------
[[ 6.80329523e+07 0.00000000e+00 -1.79715871e+07 -1.43701515e+08]
[ 0.00000000e+00 5.24834340e+10 0.00000000e+00 0.00000000e+00]
[-1.79715871e+07 0.00000000e+00 8.36456213e+10 1.72662667e+07]
[-1.43701515e+08 0.00000000e+00 1.72662667e+07 1.23762317e+10]]
[W] - Beam Compliance Matrix at the Origin
------------------------------------------
[[1.50691722e-08 0.00000000e+00 3.20155371e-12 1.74965018e-10]
[0.00000000e+00 1.90536313e-11 0.00000000e+00 0.00000000e+00]
[3.20155371e-12 0.00000000e+00 1.19558821e-11 2.04936911e-14]
[1.74965018e-10 0.00000000e+00 2.04936911e-14 8.28315446e-11]]
```
Now let's create two load cases (101 and 102) and calculate their internal loads:
```python
sc.loads = dict()
sc.loads[101] = ab.Load(My=5e6)
sc.loads[102] = ab.Load(Tx=250000, Vz=5000.0)
sc.calculate_internal_loads()
```
Next print all internal loads (which outputs a lot of data we'll not show here):
```python
sc.print_internal_loads()
```
Or access the Pandas dataframe containing these internal loads directly:
```python
df = sc.sgs_int_lds_df
```
Next plot the cross section and its properties (we'll show the segment orientations, hide legends, change the centroid , shear center and principal axis colors and use a custom figure size):
```python
ab.plot_section(sc, segment_coord=True, title='Abdbeam - Example',
legend=False, prop_color='#471365', figsize=(5.12, 3.84))
```
Finally, plot Nx and Nxy for load case 101 (we'll change the matplotlib contour palette, reduce the internal load diagram scale, and use a custom figure size):
```python
ab.plot_section_loads(sc, 101, contour_color='viridis', diagram_scale=0.7,
int_load_list=['Nx', 'Nxy'], figsize=(5.12, 3.84))
```
## License
BSD-3
## Contribute
**Abdbeam** is at its early development stages and we encourage you to pitch in and [contribute on GitHub](https://github.com/victorazzo/abdbeam). Guidelines for contributors are in the works, so stay tuned.
## Theory
For the theory behind Abdbeam, the most complete reference is:
[Victorazzo DS, De Jesus A. A Kollár and Pluzsik anisotropic composite beam theory for arbitrary multicelled cross sections. Journal of Reinforced Plastics and Composites. 2016 Dec;35(23):1696-711.](https://journals.sagepub.com/doi/abs/10.1177/0731684416665493)
These are also great references on its originating theory:
* [Kollár LP, Springer GS. Mechanics of composite structures. Cambridge university press; 2003 Feb 17.](https://www.amazon.com/Mechanics-Composite-Structures-L%C3%A1szl%C3%B3-Koll%C3%A1r/dp/0521126908/ref=sr_1_1?ie=UTF8&qid=1544936929&sr=8-1&keywords=Mechanics+of+composite+structures)
* [Kollár LP and Pluzsik A. Analysis of thin-walled composite beams with arbitrary layup. J Reinf Plast Compos 2002; 21: 1423–1465.](https://journals.sagepub.com/doi/abs/10.1177/0731684402021016928)
Note: the effects of shear deformation and restrained warping are assumed negligible in **Abdbeam**. Check the references above for more details.
نحوه نصب
نصب پکیج whl abdbeam-0.2.1:
pip install abdbeam-0.2.1.whl
نصب پکیج tar.gz abdbeam-0.2.1:
pip install abdbeam-0.2.1.tar.gz