The following factors increase stall speed:4
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When flaps are deployed at constant angle of attack the lift coefficient will:4
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An aeroplane has the following flap settings: 0°, 15°, 30° and 45°. Slats can also be selected. Which of the following selections will most adversely affect the CL / CD ratio?4
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Which type of flap is shown in the picture?4
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An aeroplane has the following flap positions: 0°, 15°, 30°, 45°. Slats can also be selected. Generally speaking, which selection provides the highest positive contribution to the CLMAX?4
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How does stalling speed (IAS) vary with altitude?4
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The aerodynamic centre of the wing is the point, where:4
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A CG location beyond the aft limit leads to:4
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The manoeuvre stability of a large jet transport aeroplane is 280 N / g. What stick force is required, if the aeroplane is pulled to the limit manoeuvring load factor from a trimmed horizontal straight and steady flight? (cruise configuration)4
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Which aeroplane behaviour will be corrected by a yaw damper ?4
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