Shock interaction effect on a flapped delta wing at M equals 8.2
RAO, D. M. /NASA, LANGLEY RESEARCH CENTER, HYPERSONIC VEHICLES DIV.,HAMPTON, VA./.
AIAA Journal ; 9 , 5 ; 985-986
1971-01-01
2 pages
Article (Journal)
Electronic Resource
English
The impact of strakes on a vortex-flapped delta wing
AIAA | 1983
|Parametric Design Study for a Blown Flapped Wing
AIAA | 2021
|A lifting line theory of the jet flapped wing
TIBKAT | 1960
|Induced rolling moment for NACA4412 plain and flapped wing
Online Contents | 2010
|Induced rolling moment for NACA4412 plain and flapped wing
Emerald Group Publishing | 2010
|