Oh, dead brain fan boi, now you maje tedbf a raptor killer.And Aero Expert Hydra how did you calculated.....
Did you put your empty head inside and it got stuck inside....
Oh, dead brain fan boi, now you maje tedbf a raptor killer.And Aero Expert Hydra how did you calculated.....
Did you put your empty head inside and it got stuck inside....
And Aero Expert Hydra how did you calculated.....
Did you put your empty head inside and it got stuck inside....
Calm down guys.Oh, dead brain fan boi, now you maje tedbf a raptor killer.
The design of TEDBF is really good. I liked it as it is not based on LCA MK2 and as I can see in the pics, the wing sweepback angle has been reduced. The location of canards and the wing is now perfect and it will do better than Rafale because the engines are going to be much more powerful than the Rafale engines. It appears to me that the wing sweep has been reduced to around 50* and when you go towards higher sweep angles on a canard-delta deisgn you get more benefits from vortices but the vortex drag also increases. I am happy to see this new design however I will still put my money on LERX-Delta-Tail design for a deck based fighter.
I do foresee that we will get to see TEDBF even in IAF service.
would it not make more sense to have twin vertical fins instead of the single?The design of TEDBF is really good. I liked it as it is not based on LCA MK2 and as I can see in the pics, the wing sweepback angle has been reduced. The location of canards and the wing is now perfect and it will do better than Rafale because the engines are going to be much more powerful than the Rafale engines. It appears to me that the wing sweep has been reduced to around 50* and when you go towards higher sweep angles on a canard-delta deisgn you get more benefits from vortices but the vortex drag also increases. I am happy to see this new design however I will still put my money on LERX-Delta-Tail design for a deck based fighter.
I do foresee that we will get to see TEDBF even in IAF service.
But why DSI ?The design of TEDBF is really good. I liked it as it is not based on LCA MK2 and as I can see in the pics, the wing sweepback angle has been reduced. The location of canards and the wing is now perfect and it will do better than Rafale because the engines are going to be much more powerful than the Rafale engines. It appears to me that the wing sweep has been reduced to around 50* and when you go towards higher sweep angles on a canard-delta deisgn you get more benefits from vortices but the vortex drag also increases. I am happy to see this new design however I will still put my money on LERX-Delta-Tail design for a deck based fighter.
I do foresee that we will get to see TEDBF even in IAF service.
because JF-17 has, so we also haveBut why DSI ?
would it not make more sense to have twin vertical fins instead of the single?
As green forum guys say. Its answer to everything.because JF-17 has, so we also have
Considering we are going to be getting this plane out, when the F-35s of the world are moving in, wouldn't a slanted twin give better over reduction in rcs compared to a single vertical? Also, my guess would be better control at low speeds, which would be required for a deck based fighter?Why complicate an aircraft that's not designed for stealth?
A twin fin design will add to the weight, cost more to develop and purchase, make it more complicated to maintain, and will need to carry more sensors due to the additional blind spots, and in exchange the reduction in RCS will not actually add to anything significant.
would it not make more sense to have twin vertical fins instead of the single?
How it this bad ? Its pretty good if you ask me. Plenty of low observable bits in that design. I do hope they get rid of the single vertical fin though.
The aircraft is being designed as a non stealth aircraft and chine doew not work for a CCC canard designI was hoping the trapezoidal design was also showed off, but I guess it's still WIP.
What do you think about a chine-trap-tail design?
I wud have loved a twin tail design in which the twin tail also acts as V-tail giving that additional control ability for higher flap angles while landing to reduce the speed and improving forward visibility for deck landings. Lower touch down speeds have lesser airframe fatigue and longer aircraft life.would it not make more sense to have twin vertical fins instead of the single?
DSI is because no aircraft in the world has been able to exceed Mach2 till date with external stores. So why create design complications which are not needed based on the performance needs. Even F-15EX which is touted to be Mach 2.5 can do so only as clean aircraft and that too for just 2.5 minutes and with A2A loads, its restricted to below Mach2.But why DSI ?
But AMCA is also getting DSI where there is a supercruise requirement.DSI is because no aircraft in the world has been able to exceed Mach2 till date with external stores. So why create design complications which are not needed based on the performance needs.
Considering we are going to be getting this plane out, when the F-35s of the world are moving in, wouldn't a slanted twin give better over reduction in rcs compared to a single vertical? Also, my guess would be better control at low speeds, which would be required for a deck based fighter?
The aircraft is being designed as a non stealth aircraft and chine doew not work for a CCC canard design
AMCA will not be able to supercruise above Mach 1.8.But AMCA is also getting DSI where there is a supercruise requirement.
I agree to your suggestion regarding the alternative design with tail.I am not referring to a CCC design. I'm referring to the alternative TEDBF design which has a trapezoidal wing and tail, no canards.
So chines + trapezoidal wing + tail, as an alternative to your LERX + delta + tail design.
I agree to your suggestion regarding the alternative design with tail.