Hello,

would like some feedback/explanation as to why that is, concerning the question :

With increasing altitude and constant IAS the static lateral stability (1) and the dynamic lateral/directional stability (2) of an aeroplane with swept back wing will:

(1) increase (2) decrease- correct answer.

My textbook only dealt with dynamic stability when considering the longtitudinal axis (pitch) and then only expanded on aerodynamic damping as an influencing factor. This question also lacked an explanation below it in the BGS database, so I am at a loss of information for the moment.

Thank you

would like some feedback/explanation as to why that is, concerning the question :

With increasing altitude and constant IAS the static lateral stability (1) and the dynamic lateral/directional stability (2) of an aeroplane with swept back wing will:

(1) increase (2) decrease- correct answer.

My textbook only dealt with dynamic stability when considering the longtitudinal axis (pitch) and then only expanded on aerodynamic damping as an influencing factor. This question also lacked an explanation below it in the BGS database, so I am at a loss of information for the moment.

Thank you

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