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YASim: Difference between revisions
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* '''midpoint:''' The location of the widest part of the fuselage, expressed as a fraction of the distance between A and B. | * '''midpoint:''' The location of the widest part of the fuselage, expressed as a fraction of the distance between A and B. | ||
* '''idrag:''' Multiplier for the "induced drag" generated by this object. Default is one. With idrag=0 the fuselage generates only drag. | * '''idrag:''' Multiplier for the "induced drag" generated by this object. Default is one. With idrag=0 the fuselage generates only drag. | ||
* '''cx,cy,cz:''' Factors for the generated drag in the fuselages "local coordinate system" with x pointing from end to front, z perpendicular to x with y=0 in the aircraft coordinate system. E.g. for a fuselage of a height of 2 times | * '''cx,cy,cz:''' Factors for the generated drag in the fuselages "local coordinate system" with x pointing from end to front, z perpendicular to x with y=0 in the aircraft coordinate system. E.g. for a fuselage of a height of 2 times the width you can define cy=2 and (due to the doubled front surface) cx=2. | ||
=== Surfaces === | === Surfaces === | ||