Question 24

AENAT1 markNeeds review
An aircraft with twin jet engines has the following specifications:
Thrust produced (per engine) = 800 N
Spanwise distance between the two engines = 10 m
Wing area = 50 m², Wing span = 10 m
Rudder effectiveness,

/deg
Density of air at sea level = 1.225 kg/m³
The rudder deflection, in degrees, required to maintain zero sideslip at 100 m/s in steady and level flight at sea level with a non-functional right engine is ______ (round off to two decimal places).

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2021AE

GATE AE 2021 · Paper 1

Aerospace Engineering · Original paper archive

Section
Aerospace Engineering
Question type
Numerical answer (NAT)
Marks
1 mark

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