A 1/13.5 scale National Aeronautical Laboratory Light Aircraft (NALLA) model was instrumented and dynamically flown with one degree of freedom. Experiments were conducted at center of gravity (CG) locations of 0.28 bar-C and 0.43 bar-C. The neutral point of the configuration was shown to be in the range of 0.57 bar-C to 0.58 bar-C, suggesting aft loading. The power effect was shown to be a pitch up above 10 degrees alpha trim and a pitch down below 10 degrees alpha.
Dynamic Flying Investigations on 1/13.5 Nalla Model (Longitudinal Results)
1991
30 pages
Report
Keine Angabe
Englisch
13.5 Finite discrete Markov model of ship safety
British Library Conference Proceedings | 2009
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