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byuflowlab
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FLOWVLM
Vortex lattice method for inviscid lifting-surface aerodynamics
GNU Affero General Public License v3.0
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Error while running the flappingwing function
#22
M4H1-K
opened
6 months ago
3
Dev
#21
EdoAlvarezR
closed
1 year ago
0
incorrect types or wrong order?
#20
skywo1f
closed
2 years ago
1
could not compile because there is no module named mpmath for julia
#19
skywo1f
closed
8 months ago
4
Tip loss corrections are a bit too aggressive, and not accessible to user.
#18
juddmehr
closed
3 years ago
1
More robust airfoil extrapolations/corrections
#17
juddmehr
closed
3 years ago
2
Airfoil data plotting
#16
juddmehr
closed
3 years ago
0
Exceeding Mach 1.0 in optimization in FLOWVLM_rotor_ccb.jl
#15
tylercritchfield
closed
3 years ago
2
Fixes #13
#14
tylercritchfield
closed
3 years ago
0
Vector/scalar addition in 1.x errors
#13
tylercritchfield
closed
3 years ago
0
output cn, ct, cl, cd for all cases.
#12
juddmehr
closed
3 years ago
1
"fixes" for issue #10
#11
juddmehr
closed
4 years ago
0
More outputs from CCBlade would be nice.
#10
juddmehr
closed
3 years ago
0
Total run time
#9
taylormcd
closed
3 years ago
0
No working release version
#8
taylormcd
closed
3 years ago
0
Lift Slope
#7
taylormcd
closed
3 years ago
0
Functions exposed to user
#6
taylormcd
closed
3 years ago
0
Additional solutions not added when calculating forces
#5
taylormcd
closed
3 years ago
0
Zero lift angle of attack
#4
taylormcd
closed
3 years ago
0
Multiple panel wing vs. single panel wings
#3
taylormcd
closed
3 years ago
0
Available fields? Output of fields?
#2
taylormcd
closed
3 years ago
0
Adding questions to documentation?
#1
taylormcd
closed
3 years ago
0