Investigation of unsteady flow past four NACA 6-percent-thick airfoil sections
1956-07-26
Miscellaneous
No indication
English
Low-speed characteristics of four cambered, 10 percent-thick NACA airfoil sections
Engineering Index Backfile | 1950
|Unsteady Compressible Flow on a NACA 0021 Airfoil
AIAA | 2011
|UNSTEADY COMPRESSIBLE FLOW ON A NACA 0021 AIRFOIL
British Library Conference Proceedings | 2011
|