Quote Lyman
having transitioned to fully Stalled with no change in Angle of Attack
Quote Dozy Wannabe
An aircraft wing cannot transition from unstalled to fully stalled without a change in AoA.
You are correct. The AOA was increasing, my point is that the a/c retained a similar and extreme AOA to and through the STALL....the entry was gentle, the last portion of the climb was due momentum, not lift, nor power.
May I replace "no change" with "no palpable change" ?
Last edited by Lyman; 3rd August 2012 at 21:25.