Swept wing aircraft liability of tip stall?


wondered why swept wing aircraft assumed more liable wing tip stall straight wing aircraft , figured research on issue today , stumbled accross site on google explains phenomenon , '' http://www.tpub.com/content/aviation2/p-1231/p-12310053.htm ''
says reason why swept wing aircraft more prone tip stall because of induced drag occurs on wing tip weakens airflow across area , hence more liable stall straight wing, in fact, considering understand induced drag , present in every aircraft , every sort of wing , straight wings no exception , should occur on straight wing aircraft how come they're assuming '' swept wing arcraft more liable tip stall straight wing '' :s im getting completly puzzled .
can explain ?

i wondered why swept wing aircraft assumed more liable wing tip stall straight wing aircraft , figured research on issue today , stumbled accross site on google explains phenomenon , ''...


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