I'm really worried about my testosterone levels at this pointChacha Vidhayak Hain Humare...View attachment 76289
It's definitely going to have huge amount of fuel and big AESA radar.
Where'd you find them? @Kuntal
And greatest aerodynamically streamlined design I've seem... Just see how the body adheres to area-ruled shape, but also the nozzles get smoothly tapered from far away.It's definitely going to have huge amount of fuel and big AESA radar.
So you're this guy right...Instead of a single vertical tail, how about going for a V-tail (like YF-23 style) or twin tail ( like mig 1.44 style).
Don't know its impact on aerodynamic performance, but it can improve stealth features. Probably, won't matter to navy since it's requirement is a twin engine 4.5 gen fighter, but it will improve the chances of air-force variant ORCA into getting inducted in sizeable numbers in IAF, who require 5th gen fighter after 2030.
Instead of a single vertical tail, how about going for a V-tail (like YF-23 style) or twin tail ( like mig 1.44 style).
Don't know its impact on aerodynamic performance, but it can improve stealth features. Probably, won't matter to navy since it's requirement is a twin engine 4.5 gen fighter, but it will improve the chances of air-force variant ORCA into getting inducted in sizeable numbers in IAF, who require 5th gen fighter after 2030.
No chance... Vertical fins are required to counter rolling tendency at high-Alpha. This limitation/complication was noted in Yf-23, which unlike F-117 was a fighter jet. And those were airforce versions.So you're this guy right...
View attachment 76520
I agree about the limitations in V-tail. But how about more conventional twin tail in canard + delta design. Like this one:No chance... Vertical fins are required to counter rolling tendency at high-Alpha. This limitation/complication was noted in Yf-23, which unlike F-117 was a fighter jet. And those were airforce versions.
Would be much more problematic in Naval scenarios, almost dangerously so.
This agone the other hand, is not needed. Mig-44, J-9B, J-20 with intakes at sides would be wide enough to need this to manage their canard vortex...I agree about the limitations in V-tail. But how about twin tail in canard + delta design. Like this one:
Area ruling is based on total volume of fighter(wing, fuselage, and combined volume at any point on fuselage length) fuselage plotted against fuselage length,@patriots @porky_kicker @Karthi @Kuntal
As far as area-ruling is concerned, TEDBF fuselage is superior to both MWF & AMCA!
View attachment 74854
I can look at Jf-17 & say it has shit area-ruling Yes, I may not have details or numbers but the "coke-bottle" shaping is far more evident.Area ruling is based on total volume of fighter(wing, fuselage, and combined volume at any point on fuselage length) fuselage plotted against fuselage length,
Only a detailed graph will give an accurate idea,
We cant determine which has superior area ruling , just by looking at scale models
Not volume.Area ruling is based on total volume of fighter(wing, fuselage, and combined volume at any point on fuselage length) fuselage plotted against fuselage length,
Only a detailed graph will give an accurate idea,
We cant determine which has superior area ruling , just by looking at scale models
Well, these are all I was waiting for since I heard the word "TEDBF"
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