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BEMT
Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering
GNU General Public License v2.0
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bemt for proprotor with aerodynamic twist (various airfoil shape along blade span)
#4
mohammadrezaaerospace
opened
1 year ago
0
Unable to run the code
#3
bbu-0078
closed
1 year ago
2
Bachelor Thesis
#2
nicolaslimajf
closed
1 year ago
2
Reference to the base theory
#1
pdkdrp
closed
2 years ago
2