Experimental determination of the effects of frequency and amplitude of oscillation on the roll-stability derivatives for a 60 degree delta-wing airplane model
1958-02-24
Miscellaneous
No indication
English
Engineering Index Backfile | 1960
|Engineering Index Backfile | 1959
|WING SWING AMPLITUDE TESTING DEVICE FOR AIRPLANE DURING DUTCH ROLL
European Patent Office | 2022
|