v1
Aerodynamic Shape Design of a Powered Helicopter Cell Using an Adjoint RANS Method with Actuator Disk Modelling
Identifier:nobleid.org/w1/20260515/3F0F2EDB
Type:Journal Article
0 views
Embeddable Badge
[](https://nobleid.org/work/w1/20260515/3F0F2EDB)
Bibliometric Analysis
Impact metrics, research fronts, co-authorship networks →
Authors & Claims