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Reduction of Vertical Tail Using Differential Thrust: Influence on Flight Control and Certification

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Academic year: 2021

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Figure

Figure 1 : Illustration of an ATR72 with distributed propulsion, differential thrust and engine failures
Figure 3: DEP ATR72 using differential thrust only and three engine failures as shown in Fig
Table 1 : Flight parameters at the studied flight conditions
Figure 4: Maximum positive and negative
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