Low-amplitude Damping-in-pitch Characteristics of Four Tailless Swept Wing-body Combinations at Mach Numbers from 0.85 to 1.30 as Obtained with Rocket-powered Models
1954-11-24
Miscellaneous
No indication
English
Engineering Index Backfile | 1954
|Control of a swept wing tailless UAv through wing morphing
Tema Archive | 2007
|Density fields around sphere at mach numbers 1.30 and 1.62
Engineering Index Backfile | 1950
|