Re: Warbirds planes
Date: 1996/05/18
Forums: comp.sys.ibm.pc.games.flight-sim
>Hawkey:
>I have been flying WBs since it came out. U seem to have info
on the performance of these birds.
>It seems impossible to get these planes to fly any faster than
330 IAS at any altitude. At 10K feet the P51D should be flying at
a minimum of 375 or according to Green it should fly at 395 TAS.
I add 2 miles per hour per 1K of altitude. Applying this to WBs P51B u get
330 IAS plus 20 fo raltitude and u get 350 TAS!!! Same for
FW190A-4 and other plances.
>I welcome your comments and analysis.
>ROland N. Cataldo
The book figures for a P-51D say 437 MPH top speed.
The ceiling is supposed to be 41,900 feet. Try it in WarBirds
and see what you get. :)
Here is the file convert.txt explaining a little bit about IAS
and TAS and how to convert. Remember WarBirds speedometers
are in MPH and they are inaccurate. For an approximation though while flying,
you can use the table. It's not as complicated as some would have you believe.
For a closer determination of top speed you can climb to the altitude you
want and time how long it takes to fly between 3 grid lines on the map.
This is a distance of 40 miles.
Example: (Distance/time in seconds) *3600=Miles Per Hour.
As far as speed being off in the P-51, it is a little slow.
A bigger concern is fuel consumption which may be off by about 30%. This
forces you to carry more weight which reduces performance. Total flight
time involving takeoff and climbing to 26k and throttling back to about
335 MPH TAS is only 1 hour and 17 minutes with half a tank of fuel.
It makes one wonder how a P-51D could have made it to Germany and back,
even with drop tanks, at this rate of fuel consumption. The ceiling is also
lower then book figures with the P-51 in WarBirds.
Here is the table you can use with the speedometer.
AIR SPEED CONVERSIONS
The following table facilitates IAS to TAS, TAS
to IAS conversions. Simply multiply IAS, or divide TAS
by th altitude factor to convert. This lets you compare data between games,
or to real world data.
A circular slide rule type flight computer was used to obtain data. Density
altitude was set to desired altitude and TAS was read from IAS.
In other words density altitude and pressure altitude were assumed to be
equal. You can read the temperature at which this happens off "whiz
wheel" opposite pressure altitude. True altitude is very, very close
at this setting. This is what I believe Microprose did to get the factors
used in their text file. TAS was divided by IAS to calculate
"altitude factor."
Numbers in parenthesis are from Microprose file f15spd.txt.
Differences are probably due to: my 50 year old eyes, differences in
E-6B flight computers, and the difficulty in reading a non-precise device
like a mechanical circular slide rule. I used reading glasses AND a magnifying
glass. If anyone finds any glaring errors, let me know.
Jeffrey Dillman
Alt. factor Alt. factor
1k 1.017 21k 1.394
2k 1.031 22k 1.417
3k 1.047 23k 1.443
4k 1.063 24k 1.470
5k 1.078 (1.077) 25k 1.497
6k 1.097 26k 1.523
7k 1.113 27k 1.551
8k 1.130 28k 1.576
9k 1.149 29k 1.609
10k 1.167 (1.164) 30k 1.634 (1.635)
11k 1.186 31k 1.669
12k 1.203 32k 1.697
13k 1.223 33k 1.733
14k 1.244 34k 1.763
15k 1.263 35k 1.798
16k 1.286 36k 1.833
17k 1.303 37k 1.880
18k 1.329 38k 1.923
19k 1.349 39k 1.970
20k 1.373 (1.370) 40k 2.018 (2.016)
Jeffrey Dillman |