Experimental determination of the effects of frequency and amplitude of oscillation on the roll-stability derivatives for a 60 degree delta-wing airplane model
24.02.1958
Sonstige
Keine Angabe
Englisch
Engineering Index Backfile | 1960
|Engineering Index Backfile | 1959
|WING SWING AMPLITUDE TESTING DEVICE FOR AIRPLANE DURING DUTCH ROLL
Europäisches Patentamt | 2022
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