Apparently the leading edge curves downward near the nose. I assumed the wing's leading edge was a straight line all the way to the tip of the nose. Also, the side facing IRST-windows (?) are apparent on top of the nose as well.

Edit: Higher resolution image inserted
CAC_J-36_A_011.PNG
 
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Apologies if someone has already made this observation. I read a mention in another thread about canards and other devices being potentially used to help with control authority in an engine-out situation on a tailless aircraft. It got me to wondering if maybe the third engine was a mitigation here for that eventuality. I don't think it's the only, or primary driver, but it may have figured into the design.
 
Apparently the leading edge curves downward near the nose. I assumed the wing's leading edge was a straight line all the way to the tip of the nose. Also, the side facing IRST-windows (?) are apparent on top of the nose as well.

View attachment 764125
As part of your artistic impression, did you just copy paste the nose section from your Kaan(?) sketch? :D

kaan.jpg
 
Apologies if someone has already made this observation. I read a mention in another thread about canards and other devices being potentially used to help with control authority in an engine-out situation on a tailless aircraft. It got me to wondering if maybe the third engine was a mitigation here for that eventuality. I don't think it's the only, or primary driver, but it may have figured into the design.

Post in thread 'Shenyang / Chengdu "6th Gen" Aircraft - News and Analysis' https://www.secretprojects.co.uk/th...-aircraft-news-and-analysis.40872/post-744318
 
I've played around with Solidworks motion study a bit... Unfortunately the upload of the animated GIF doesn't work :(
Save your gif as an mp4 or any other movie file and upload on YouTube

Notice that old version of Solidworks can't export mpeg or mp4 compatible with modern players but FLV or window player classic.

So Motion study to Mpeg - > Mpeg to mp4 - > upload or share the file
 
Save your gif as an mp4 or any other movie file and upload on YouTube

Notice that old version of Solidworks can't export mpeg or mp4 compatible with modern player but FLV or window player classic.

So Motion study to Mpeg - > Mpeg to mp4 - > upload or share the file
Thx for the hint. Problem already solved!
Actually I saved the motion study as mp4, then convert it to gif to be able to share it directly in the post.
 
Apologies if someone has already made this observation. I read a mention in another thread about canards and other devices being potentially used to help with control authority in an engine-out situation on a tailless aircraft. It got me to wondering if maybe the third engine was a mitigation here for that eventuality. I don't think it's the only, or primary driver, but it may have figured into the design.
I don't believe so. I think that the third engine is partly because it's a huge 45+ ton aircraft, and partly because the onboard systems need a huge amount of electrical power generated.
 
Apparently the leading edge curves downward near the nose. I assumed the wing's leading edge was a straight line all the way to the tip of the nose. Also, the side facing IRST-windows (?) are apparent on top of the nose as well.

Edit: Higher resolution image inserted
View attachment 764180


Indeed ... you should modify your CG

J-36 front.jpg
 
Indeed ... you should modify your CG

I know, but there are many unknowns and that's not the only inaccuracy of the model. I'll wait until more details come to light and then possibly rework the model from scratch. For now, it's good enough to get a better idea of the overall concept.
 
Can anyone confirm, the J-36 is in the air again right now? Just got a hint from a friend ....
 
So, for yaw control, they channel the Delta extrados vortex asymmetrically.

I would be surprised if that work well at high alpha (20deg+). This would confirm this is an attack plane. A serious one.

Notice also how fast it lands despite the large wing area. (and w/o apparently any much flaps extended)
 

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