Effect of Reflex Camber on the Aerodynamic Characteristics of a Highly Tapered Moderately Swept-back Wing at Reynolds Numbers up to 8,000,000
1947-03-01
Miscellaneous
No indication
English
Engineering Index Backfile | 1947
|Reynolds number effects on flow characteristics and aerodynamic performances of a swept-back wing
Online Contents | 2011
|Swept-tapered-wing aerodynamics
NTRS | 1976
|