What is the position of the elevator in relation to the trimmable horizontal stabiliser of a power assisted aeroplane that is in trim?4
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By what percentage does VA (EAS) alter when the aeroplane's weight decreases by 19%?4
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If you decrease the propeller pitch during a glide with idle-power at constant IAS the lift to drag ratio will:4
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Drag is in the direction of - and lift is perpendicular to the:4
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The forces of lift and drag on an aerofoil are, respectively, normal and parallel to the:4
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How are the speeds (shown in the figure) at point 1 and point 2 related to the relative wind / airflow V?4
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The lift- and drag forces, acting on a wing cross section:4
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Which point shown in the figure corresponds with CL for minimum horizontal flight speed?4
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The span-wise flow is caused by the difference between the air pressure on top and beneath the wing and its direction of movement goes from:4
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Which of the following wing planforms gives the highest local lift coefficient at the wing root?4
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