Numerical analysis of a NACA0012 airfoil with leading edge ice accretions
25th AIAA Aerospace Sciences Meeting ; 1987 ; Reno , NV , U.S.A.
1987-01-01
Conference paper
Electronic Resource
English
Leading-Edge Parametric Study of the NACA0012-IK30 Airfoil
TIBKAT | 2022
|AIAA | 1997
|NTIS | 1997
|