OK guys, here is my theory.
OK the last Radar fix has QZ8501 at a Ground Speed of 363Knots at 36300FT and climbing.
Quite possibly, the aircraft had penetrated a CB cell before this point which it was trying to avoid by climbing and diverting West of Track.
The aircraft was already in a lot of trouble.
The Turbulence Penetration Speed is 270KIAS (knots indicated) - this speed needs to be corrected for pressure altitude of 36300FT
I will assume that the Corrected Airspeed (CAS) and Indicated Airspeed (IAS) are the same.
Now:
TAS = IAS/sqrt(delta)
Delta = Ratio of Air Density to International Standard Atmosphere Sea Level Pressure = 270/(T+273.15) * (P/1013.25)
P= Ambient pressure in HPa(mB)
T= ambient temperature in degrees celsius
Now, pressure adiabatic lapse rate at 36300FT gives us an Ambient P of 225hPa
Ambient Outside Air Temperature is -56.5 degrees celsius - T = -56.5
The above is assuming normal International Standard Atmosphere Adiabatic Lapse rates.
http://weatherfaqs.org.uk/book/export/html/174Therefore: 270/(-56.5+273.15) * (225/1013.25)
therefore TAS = 75knots
Therefore at Turbulence Penetration Speed, the aircraft was about to enter a DEEP Stall and drop from the sky like a shower of shit! (sorry about the crudeness).
My calculations do not take into consideration CAS, or actual lapse rates because these are the unknowns until we recover the Black box.