Tests made in Langley free flight tunnel at lift coefficient of 1.0, covered range of geometric dihedral angles from -- 20 to 20° and range of vertical tail areas from 0 to 15% of wing area; results compared with previously reported results of similar series of tests on conventional model having wing with aspect ratio of 6.
Lateral stability and control characteristics of free-flying model having unswept wing with aspect ratio of 2
Nat Advisory Committee Aeronautics -- Tech Note
1948
30 pages
Report
Englisch
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