Gripen,
Please, show us how did you reach 0,1296.
I actually sat down and started workin your numbers Gripen. Then I realized that you are using different numbers for Cl and factoring in what you say is the "Clo".
Bottom line is what the NASA engineer said about a formula YOU SAID COULD BE NOT BE USED for 2D data but ONLY CALCULATES 3D!!
You THINK you know what the formulas are used for AND everything that has to be factored in but the FACTS are you don't. Neither do I know everything, I am not an aeronautical engineer.
Therefore it is totally pointless to argue numbers at our level especially when those number ONLY apply to a specific flight condition with all other parameters being equal.
Leave that to the folks who do know. HTC will figure out the data they need.
In practical terms it's a stupid debate. Please either join the discussion or you can go start a new thread and rant about your calculations.
Phookat,
That is the whole point. The FW-190A gained Horsepower and weight accordingly to increase performance over its lifespan. . By tracking the weight gain and motor derating we can see this.
Why would anyone produce a version of the same fighter when they have a better performing version already in service, factories already tooled, and workers already producing a better performing product? It does not make sense.
Sticking to what we can prove.
1. The popular notion the FW-190 gained tons of weight and lost lots of performance is not true.
Just look at the FW-190A5 level speed chart that has been adjusted for air density differences.
The FW-190A8 level speed chart is not adjusted so we don't know the exact conditions it occurred. It gives us an idea and falls within the 190A5 density corrections.
http://www.terra.es/personal2/matias.s/fw190.htm2. We know for a fact level speed, climb rates, climb speeds, and many of the performance parameters of the Aircraft. However these facts only come from a few sources. Since Allied A/C have much data available on each type it is easier to pick and choose the best data. Example - 4th Fighter group Spitfire site notes the wide variation in performance amoung the fighters of the same type in many of its test.
Another example is the test pilots at Rechlin testing the FW-190D9 produced different results with each test flight based on Engine condition, prop maintenance, air density, etc. all from the same plane/engine type. Their results varied as much as 15km/hour at full throttle height.
3. Performances factors we don't know for a fact can be deducted by analyzing the tactical trails and thru deductive reasoning produce a fairly accurate approximation of those parameters.
Tactical trials out there are:
P47
F4U
Hellcat
Spitfire Mk V
Spitfire Mk IX Merlin 61
If anyone is missing one of them please let me know.
The Zeke tactical trials give a great reference for how much or little makes a difference in combat.
I have that one too if it is needed.
Crumpp