The diagram shows the parameter X versus TAS. If a horizontal flight is considered the axis X shows4
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On a swept wing aeroplane at low airspeed, the 'pitch up' phenomenon:4
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On a wing fitted with a 'Fowler' type trailing edge flap, the 'Full extended' position will produce:4
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The function of the slot between an extended slat and the leading edge of the wing is to:4
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What increases the stalling angle of attack ? Use of:4
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A slat will:4
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To be able to predict compressibility effects you have to determine the:4
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'Tuck under' is caused by (i) which movement of the centre of pressure of the wing and (ii) which change of the downwash angle at the location of the stabilizer.4
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Air passes a normal shock wave. Which of the following statements is correct?4
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When the air has passed through a normal shock wave the Mach number is4
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