Look on Bombardier's, ATR's and Embraer's web site for some excellent charts on turboprop efficiency.
The speeds of these airplanes are effected so much by IAS / TAS that I am not sure how you are going to correlate your data. Generally you can convert IAS to TAS by multiplying IAS by ( 1 + (FL * .02 ))
For example the profile of the CRJ200 at my operator is:
Airspace restricted to 10,000 feet ( 200 / 250 / 290 ) depending on which airport you depart. Usually 250 KIAS to 10,000 feet. Figure 3,600 per hour burn climbing at 2 to 4,000 FPM
Accelerate to 290 KIAS and hold that to cruise altitude. Climb rates drop off to 1,500FPM all the way down to the ATC required 500FPM. 290KIAS at FL300 is 464 True airspeed, ( 290*1.6 which is about 9 knots faster than reality, but close enough ) at 2,800 to 3,000 pounds per hour. This is our cruise speed and we prety much cruise within a couple percentage points of our climb power setting. The CRJ200 seems to always be around 450 to 455 knots true airspeed.
Decent - within 10 knots of limitations ( 330 to 335 KIAS ) 480 KTAS to 10,000 feet, then as restricted by airspace. Fuel burns probably drop to something less than 1,200 pounds per hour.
Of course there are a bunch of other considerations. How long do the engines last? The DO328J's were going through engines with less than 2,000 hours on them, while some ATR operators have gotten 15,000 hours between engine removals. Also, the jets' speed means you can get more flight legs out of your airplanes every day. With ASA it is thought that the Dash 8 Q 400 was simply too big for the congested ramp space at the Atlanta airport and with any airplane you have to consider the costs of an additional training department, spares and mechanics.
If you get all of this worked out, let us know. If you want to cheat, you can buy the data from Conklin and DeDekker.
Regards,
~~~^~~~