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Diseño preliminar y análisis tecno económico de un avión personal

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Figure

Figure 1.1 Principal aspects for design an aircraft. [61]
Figure 1.12 shows an aircraft in steady and level flight at cruising speed.
Figure 1.13 Aircraft cost factors. [46]
Table 1.8 Principal data for small helicopters.  Helicopter  type  Engine  Gross  weight  [kg]  Lift  power [Kw]  Power  loading [kg/kW]  Main  rotor  diameter [m]  Heli-Sport  CH-7 [22]  Rotax 914UL  450  85  5.3  6.2  LCA LH 212  Delta [26]  Rotax 914  4
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