Depth of the weapons bay for J-35 is unknown as there are not good images. Depth of J-20's bay can be estimated from images and is not shallow one bit. It looks deep enough to house 500 kg bombs easily and even 1000 kg weapons, if in a somewhat different shape than JASSM missile, for example. When looked at from the side, J-35 is quite a bit more slender than J-20 and it's in my opinion highly questionable if depth of J-35s bays can match J-20s. So... I'd say this is a variable where either J-20 is better or two planes are similar.
I would really advice against gauging dimensions by eye. Fuselage height only tells one part of the story.
What I've heard is that the J-20 actually cannot fit 500 kg bombs in its IWB due to the intakes taking up some of the frontal section of the bay.
See how the intakes take up some space? The aft section of the bay is deep enough, but not the front. 1000 kg bombs are definitely out of the question.
The J-35/A, since it uses medium-thrust class engines, can afford thinner intake ducts and thus the front part of the bay wouldn't be as obstructed. 1000 kg bombs are still out of the question, but 4 500 kg bombs are possible. The J-20 uses high-thrust class engines and they require much thicker ducts due to the higher overall mass flow.
Hence, the J-20's fuselage may appear thicker, but much of that is dedicated to the s-ducts instead of the IWB.
Then the most important metrics. Payload and range. Which are often interdependent, as bigger payload reduces range. J-20 is a bigger plane with more lift and same payload doesn't impact it as much as it does a smaller plane like J-35.
That's only one part of the equation. The J-35/A is a (much) lighter airframe.
J-20 has a lot of internal volume for a lot of fuel. J-35 is much more slender and my estimates of internal volume of both planes suggest to me it holds even less fuel per kN of thrust generated than J-20.
That's not how it works. The range of an aircraft depends on
the percentage of the aircraft dedicated to fuel instead of the fuel mass itself.
J-35 has so far not been seen with any external fuel option.
By that logic, the extensive application of additive manufacturing used on the J-35/A is also unconfirmed to be utilised on the J-20A, much less legacy J-20s.
And even if it does have one, it's highly unlikely it will be able to haul around four 600-gallon tanks like J-20.
Does it need to? Look, I don't know why you're hellbent on comparing the stats of a heavyweight air superiority fighter to a medium-sized multirole fighter. Obviously a bigger platform is gonna look more appetizing on paper. But the point of the J-35A isn't to match the J-20's range. It might, but that's not its main design purpose.
The J-35A's point is to provide and enhance multirole capabilities of the PLAAF so that the J-20 can focus on air superiority. Why have the J-20 conduct stealth A/G strikes when you can just get a cheaper, potentially even stealthier platform to do it.? The J-20s are supposed to penetrate the enemy's "web" and establish air superiority while the J-35As construct the "web" on the friendly side and provide multirole support.
It doesn't need to match the J-20's range and powerful radars. That's not the point of the platform.
Basically, whatever payload J-35 will be able to hold, J-20 should be able to at least match it.
I've said why that might not be the case. Blame the WS-10C/15's overall mass flow.
When adding external weaponry, J-20 should have even greater payload advantage. And whatever the payload, J-20 will be able to carry it to longer distances.
And why do that when you've got J-16s? I get it if air superiority was established and it's AAMs that the J-20 is carrying externally. But for A/G missions it's makes much more sense to shove it to J-16s (if air superiority was established) and/or J-35A (in contested airspace).
Again, the J-35A doesn't need to carry it as far as the J-20. It could, but that's again not the main goal.
Right now, the only advantage that may be is the integrated optical/thermal targeting system. We know that current J-20 variants can't really look much past the forward quadrant. We don't know if current J-35 are similar but still possible its system is designed to look to the sides, like F-35's is. But even if that's all true, it doesn't really tell us anything about future J-20 and J-35 variants.
If both uses hybrid EOTSs, that's fine. But if such tech isn't mature yet, the J-35A in theory would use MWIR EOTS for multirole strikes while the J-20 uses LWIR for air superiority.
And then there's radar targeting. J-20 is constantly being modernized with newer electronics so there's no reason to think J-20s radar and avionics are worse than J-35's. So all other things being equal, J-20's bigger radar array and more power should lead to more sensitivity and better synthetic images of land targets. Again useful in air ground strike missions.
And the J-35A should be able to match most of its prowess while being cheaper to maintain and easier to operate. Refer to above also about the distinction between MWIR/LWIR and how the J-35A would be much more suited for A/G strikes.
I guess if J-35 really had superior stealth to J-20, that might make it more useful for ground strikes than J-20 in SOME instances.
Well, the J-35/A does have an actual paper of an internal cannon.
But there's really no way of measuring stealth of those two planes so that discussion would be pointless.
Look, although the J-20's size and canards doesn't mean it can't be as stealthy as smaller, conventional wing platforms, the J-35/A is literally the closest you can get to textbook perfect. Inherently smaller airframe, no protruding control surfaces, DSI, completely smooth belly, etc. It is inherently a stealthier design.