Maximum sideslip angles and vertical tail loads computed and compared with those obtained from two other dynamic maneuvers, rudder kick and rolling pull-out; method given for computing maximum sideslip angles when forces and moments are non-linear functions of sideslip.
Sideslip angles and vertical-tail loads developed by periodic control deflections
Nat Advisory Committee Aeronautics -- Tech Note
1948
62 pages
Report
English
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Sideslip angles and vertical-tail loads in rolling pull-out maneuvers
Engineering Index Backfile | 1947
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