PPRuNe Forums - View Single Post - Why do aircrafts support less G´s in the negative side?
Old 5th Dec 2016, 21:01
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portsharbourflyer
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Load cases are a mix of "mission" cases (ie: what you want the aircraft to do, aerobatics, fighter aircraft) and the regulatory cases (CS23 and CS25 will specify, gust cases, rolling cases etc). It may the case that designing for one of the regulatory cases can result in a structure that is capable of reacting more negative g than you necessarily need for the "mission profile".
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