Results of tests made in Langley free flight tunnel on free flying dynamic model.
Experimental determination of effects of dihedral, vertical-tail area, and lift coefficient on lateral stability and control characteristics
Nat Advisory Committee Aeronautics -- Tech Note
1946
24 pages
16 Supp sheets
Report
English
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Study of effects of vertical tail area and dihedral on lateral maneuverability of airplane
Engineering Index Backfile | 1941
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