Pressure distribution measurements on semi-span rectangular wing model.
Flow about section of finite-aspect-ratio NACA-0018 airfoil on transonic bump
NACA -- Tech Note
1953
30 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Aeroacoustics of NACA 0018 Airfoil with a Cavity
AIAA | 2018
|Experimental Analysis of Implementing Roughness on NACA 0018 Airfoil
Springer Verlag | 2018
|