PPRuNe Forums - View Single Post - Relationship between Flaps / Lift Coefficient
Old 21st November 2005 | 22:18
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redsnail

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From: Duit On Mon Dei
The JAA exam answer for the super stall question is "swept wings".

Handling the Big Jets say both swept and T tails are involved. Unfortunately, DP Davies didn't write the exam paper. (A bit difficult now)

Having flown both the T tails (Dash 8) and a swept wing (HS125) I know they are both susceptible to the deep stall phenonema. Hence both fitted with stick shakers and stick pushers.

A straight winged aircraft isn't susceptible to a deep stall unless it has a T tail. That is, it does behave in a normal way with the stall untill the disturbed air blankets the tail and thus renders it useless in recovery. The pusher prevents you from going that far.

A swept wing aircraft is susceptible to a deep stall. Tail position isn't as important.

There was a brilliant discussion about this a couple of years ago on this site (possibly this forum).

I'll let the more learned folks explain the guts of it.
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