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Question
An aircraft is trimmed straight and level at true air speed (TAS) of 100 m/s at standard sea level (SSL). Further, pull of 5 N holds the speed at 90 m/s without re-trimming at SSL (air density = 1.22 kg/m3). To fly at 3000 m altitude (air density = 0.91 kg/m3) and 120 m/s TAS without re-trimming, the aircraft needs
Options:
A .  1.95 N upward force.
B .  1.95 N downward force.
C .  1.85 N upward force.
D .  1.75 N downward force.
Answer: Option B


-NA-



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