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Vortex-Step-Method
Vortex Step Method
MIT License
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42 matching stall predictions of test v3 using polar or polynomial data
#44
jellepoland
closed
5 days ago
0
Making sure this is up to speed with develop
#43
jellepoland
closed
5 days ago
0
Matching stall predictions of test_v3 using polar or polynomial data
#42
jellepoland
closed
5 days ago
0
Aerodynamic forces incorrectly calculated
#41
ocayon
closed
6 days ago
0
test_swept_wing
#40
jellepoland
closed
6 days ago
0
Make code robust against right to left geometry definition
#39
ocayon
opened
1 week ago
0
31 implement an provided based spacing
#38
jellepoland
closed
1 week ago
0
36 clean up src code after major reference frame enu induced changes
#37
jellepoland
closed
1 week ago
0
clean_up_src_code_after_major_reference_frame_ENU_induced_changes
#36
jellepoland
closed
1 week ago
0
Verify NEW AIC with U_2D calculation, the pytest is also changed
#35
jellepoland
closed
6 days ago
0
Fix that the correct averaged panel width is used, instead of the bound width
#34
jellepoland
opened
1 week ago
0
pytest the entire geometry creation, by comparing to the old "create_geometry_general" function and creating the same dict outputs
#33
jellepoland
closed
1 week ago
0
Write a plot function, that will show the forces per panel
#32
jellepoland
opened
1 week ago
0
Implement an provided-based-spacing
#31
jellepoland
closed
1 week ago
0
Implementing calculate_results functions
#30
jellepoland
closed
1 week ago
1
Add artificial functionality back, to handle stall cases
#29
jellepoland
opened
2 weeks ago
0
Documentation of Panels
#28
jellepoland
opened
3 weeks ago
0
Documentation of Filaments
#27
jellepoland
opened
3 weeks ago
0
test v3
#26
ocayon
closed
6 days ago
0
Test curved wing
#25
ocayon
closed
1 week ago
0
Test elliptical wing case Master Thesis
#24
ocayon
closed
1 week ago
1
Test 3 panel from Master Thesis
#23
ocayon
closed
2 weeks ago
1
Test panel
#22
ocayon
closed
2 weeks ago
0
Test all filament individually (review at least once more)
#21
ocayon
closed
3 weeks ago
0
Test Gamma Distribution
#20
ocayon
closed
6 days ago
1
Find the bug that causes a non-symmetrical result after iterating
#19
jellepoland
closed
3 weeks ago
1
Can the VSM handle misalgined airfoil/ribs/sections, and if not should it have an additional input, like a vector for the orientation?
#18
jellepoland
opened
3 weeks ago
0
Allow a geometric LEI airfoil input
#17
jellepoland
closed
2 weeks ago
0
Wing aero
#16
ocayon
closed
1 month ago
0
intermediate commit, leaving the liveshare
#15
jellepoland
closed
1 month ago
0
Implement a geometric alpha calculator
#14
jellepoland
opened
1 month ago
0
Allow a polynomial aerodynamic input
#13
jellepoland
closed
2 weeks ago
0
Implement a default inviscid polar
#12
jellepoland
closed
2 weeks ago
0
Dynamic Relaxation Factor Implementation
#11
jellepoland
opened
1 month ago
0
initial horshoe class setup
#10
jellepoland
closed
1 month ago
0
Merge pull request #3 from ocayon/develop
#9
jellepoland
closed
1 month ago
0
Merge pull request #2 from ocayon/develop
#8
jellepoland
closed
1 month ago
0
VSMclass
#7
jellepoland
closed
1 month ago
0
Panel class
#6
jellepoland
closed
1 month ago
0
Restructure code
#5
jellepoland
closed
1 month ago
0
Restructure code
#4
jellepoland
closed
1 month ago
0
Restructure code
#3
jellepoland
closed
1 month ago
0
Restructure code
#2
jellepoland
closed
1 month ago
0
Add aero damping, update license files
#1
ocayon
closed
10 months ago
0