DO NOT MOVE ON TO THE NEXT PAGE WITHOUT ATTEMPTING THIS QUESTION! Consider an ...
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DO NOT MOVE ON TO THE NEXT PAGE WITHOUT ATTEMPTING THIS QUESTION!
Consider an aircraft with the following take-off specification:
- Take-off field length = 1.9 km
- CLmax (at take-off) = 2.03
- Throttle setting = 98%
- Weight at take-off = 0.97 MTOW
- Ambient density = 0.954 ISA sea-level value (you'll need to go to the Working sheet here)
Q1 Calculate the Tsls/MTOW required to meet this take-off constraint at a design wing loading (MTOW/Sref) of 9,000 Pa. Give your answer to 3 d.p..
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