22.22.18 Describe the forces acting during a manoeuvre in the looping plane
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22.6.22 Describe how TR varies with increasing angle of attack ().
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22.6.24 Define the TR components lift and drag.
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22.8.2 Identify the factors affecting lift (low-subsonic speed airflow)
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22.8.4 State the lift formula, and the three basic functions contai
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22.24.18 Describe asymmetric blade effect.
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22.24.20 Explain the terms power absorption and propeller solidity.
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22.26.4 Differentiate between stability and controllability.
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22.26.10 Define lateral stability and explain the factors affecting i
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Sweep-Back / Lateral Stability
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22.8.6 Describe the meaning of the term, coefficient of lift (CL).
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22.8.8 Given a typical CL versus Angle of Attack curve for a GP-type aerofoil, i
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22.8.10 Explain the meaning of a high CLmax.
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22.8.12 With respect to the CL curve, describe the effect of:
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22.8.14 Describe three-dimensional flow over a wing and explain how
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22.26.16 With respect to stability and control on the ground, explain
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22.28.4 Explain the factors affecting yawing and rolling moments.
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22.28.8 Recall immediate actions and techniques for identifying the
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22.30.2 Define specific air range (SAR)
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22.30.2 Define Specific Fuel Consumption (SFC)
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22.32.2 Define:
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22.8.16 Explain the effect of induced downwash on α
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22.8.18 Define aspect ratio (AR) and describe the effect of AR on CL
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22.10.2 Identify and explain the components of total drag.
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