4 For A Jet Aircraft In Take Off Configuration At 0 M Isa P 1 225kg M The Following Data As Indicated In The Table B 1 (46.17 KiB) Viewed 44 times
4. For a jet aircraft in take-off configuration at 0 m ISA (p=1.225kg/m³) the following data as indicated in the table below are known: T W S Ae C₁ Соо [-] [kN] [kN] [m²] [-] 735 2635 442 0.075 8.74 2.35 [7pt.] Using the circular arc method calculate the distance from lift-off up to screen height hs. max VLOF/VMIN [-] 1.20 n [-] 1.15 hs [m] 15 Yc 10
4 Please read carefully what is asked! In this case only the airborne part from take-off to screen height needs to be calculated! V_LOF=77.15m/s R=4053m The climb angle is given, so there is no need to calculate it from equilibrium (if you did you should get 10deg anyway) And we need to check where this leads us in terms of height h_t=61.6m>h_s => gamma_s=4.93deg s=348m
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