cabatli_53
ELITE MEMBER
- Joined
- Feb 20, 2008
- Messages
- 12,808
- Reaction score
- 62
- Country
- Location
TAI has purchased a super computer having 10,000 core. New monster is going to be used for detail design/analyse of TF-X and other aircraft projects.
Follow along with the video below to see how to install our site as a web app on your home screen.
Note: This feature may not be available in some browsers.
Could be the NEC Sator.TAI has purchased a super computer having 10,000 core. New monster is going to be used for detail design/analyse of TF-X and other aircraft projects.
is there any image of the computer ?TAI has purchased a super computer having 10,000 core. New monster is going to be used for detail design/analyse of TF-X and other aircraft projects.
There is so much misinformation here. Data of TFX in the chart is given in maximum thrust, while the others are given in dry thrust. (Note that the 20000 lbf in this chart most probably refers to EJ200 or similar)
New Recruit
TF-X:
Lenght 19m (60ft)
F22:
Lenght 18.92m (62ft)
There is so much misinformation here. Data of TFX in the chart is given in maximum thrust, while the others are given in dry thrust. (Note that the 20000 lbf in this chart most probably refers to EJ200 or similar)
For this chart to make sense either TFX engine thrust should be changed to 2x13500 lbf (assuming EJ200 or similar class is still being considered) or F-22 should be changed to 2x35000 lbf, F35 to 43000 lbf and etc.
Also note that Temel Kotil said the maximum thrust of the new engine will be 27000 lbf. That doesn't even come close to the 35000 lbf of the F-22 and thus TFX will not be the fighter with most thrust in its class.
Here is a summary depending on engine choice:
TFX 2x27000 lbf (assuming new engine) or 2x20000 lbf (assuming EJ200)
F-22 2x35000 lbf
F-35 1x43000 lbf
Well I doubt that the 27000lb is meaningless. It must refer to something. Either dry or maximum thrust.He said "Turkey works on it's own engine with 27000lbs thrust" he never said something about dry or maximum thrust.
From Wikipedia:
EJ2x0
Stage 1:
Stage 2:
- The EJ2x0 with 20% growth compared to the original EJ200. The EJ2x0 engine will have dry thrust increasing to some 72 kN (or 16,200 lbf) with a reheated output of around 103 kN (or 23,100 lbf).
- The new engine plan to increase the output 30% more power compared to the original EJ200. The engine will have dry thrust of around 78 kN (or 17,500 lbf) with a reheated output of around 120 kN (or 27,000 lbf).
I will quote myself.Well I doubt that the 27000lb is meaningless. It must refer to something. Either dry or maximum thrust.
Usually when an engine is said to be of X thrust, maximum thrust is implied. Nobody classifies afterburning engines according to their dry thrust.
TAI has purchased a super computer having 10,000 core. New monster is going to be used for detail design/analyse of TF-X and other aircraft projects.