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Refinement and analysis of concept

Refinement and analysis of concept

Refinement and analysis of concept

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航空宇航学院<br />

<strong>Refinement</strong> <strong>of</strong> aerodynamics design<br />

• Control/stabilizer surface<br />

– Outer ailerons on high aspect ratio sweptback wings may<br />

introduce aeroelastic difficulties when used at high speed, <strong>and</strong> to<br />

overcome this problem alternative high speed roll control may be<br />

provided in the form <strong>of</strong> inboard ailerons or differential longitudinal<br />

controls such as tailerons.<br />

– In the case <strong>of</strong> inboard ailerons there will be an effect upon the<br />

extent <strong>of</strong> the trailing edge flaps although this may be minimised<br />

by locating the controls immediately behind powerplants.<br />

– Within some limits the effectiveness <strong>of</strong> trailing edge devices may<br />

be adjusted by variation <strong>of</strong> their chordwise extent.<br />

Aircraft Conceptual Design

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