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By E. Obert

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14 - Take-off profile. Source : AGARD LS-43, paper no. 7 22 5)&"*3$3"'5%&4*(/130$&44t Landing Climb requirements have not only been formulated for take-off but also for landing. 15. 7% at the certificated minimum approach speed. 2%. When an engine failure occurs during flight it is possible to have a missed approach when approach flaps have been selected, but a go-around should not be attempted when landing flaps are deployed. Once landing flaps are selected the landing must be continued .

18 - Basic take-off framework. Source: AGARD LS-56, paper no. 19 - Engine thrust decay with speed. Source: AGARD LS-56, paper no. 21 - Take-off ground run. Source: AGARD LS-56, paper no. 20 - Take-off distance to screen. Source: AGARD LS-56, paper no. 22 - Take-off flare-up. Source: AGARD LS-56, paper no. 23 - Basic landing framework. Source: AGARD LS-56, paper no. 24 - Landing distance. Source: AGARD LS-56, paper no. 25 - Statistical correlation of the unfactored landing distance. Source: E. 26 - Elementary kinematic relations.

There are various requirements on the design such as the Take-Off Field Length (TOFL), the Engine-Out Altitude (EOA) and the approach airspeed. 7 - EET Baseline design selection chart. optimized by choosing a certain Source: AIAA Paper No. 79-1795 design point are the Minimum Block Fuel (MBF), the minimum Direct Operating Costs (DOC) and the minimum Take-Off Gross Weight (TOGW). Where the design point is chosen depends on expectations of fuel prices, inflation, purchase price, number of aircraft to sell, etc.

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