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