Chengdu next gen combat aircraft (?J-36) thread

Steven D

New Member
Registered Member
So the bottom part of the nozzle aren’t so much nozzle petals as they are flaps…
Disagree, imo this is a combination of yf23 style nozzle and 2D TVC.

From a fluid dynamics point of view, flaps are to induce changes of air flow field arround an aerofoil. The flow field arrond the bottom surfaces of nozzle is dictated by engine exhaust, not free airflow arround an aerofoil, so I don't expect it to have any aerodynamic effect similar to a flap.
 

asif iqbal

Banned Idiot
J36 for high altitude high speed precision strike on enemy bases like Guam

can imagine V- formation of J36 for deep strike

JXX for Carriers
 

ACuriousPLAFan

Brigadier
Registered Member
I’m sorry, the search functions doesn’t seem to be working. The author should be Tao Chenggang, deputy chief designer of the AVIC Chengdu Aircraft Design and Research Institute.

Here is a figure though..

View attachment 150552

That model is pretty generic, likely taken from that NASA simulation back from the 1990s. Certainly doesn't illustrate J-36.

Giving the size it more like a bomber

I don't think the illustration is meant to be accurate. More of a representative function.
 

by78

General
A short video.


54471372220_5ba1b56d12_4k.jpg
 
Last edited:

cdj20

New Member
Registered Member
I’m sorry, the search functions doesn’t seem to be working. The author should be Tao Chenggang, deputy chief designer of the AVIC Chengdu Aircraft Design and Research Institute.

Here is a figure though..

View attachment 150552
The figure is from the paper
Please, Log in or Register to view URLs content!

1745419395086.png
The authors are from
  1. Nanjing University of Aeronautics and Astronautics, College of Automation Engineering
  2. Chengdu Aircraft Design & Research Institute (or AVIC Chengdu Aircraft Design & Research Institute)
  3. Nanjing University of Aeronautics and Astronautics (NUAA)
None of them is from AVIC.

The model is the ICE proposed by Lockheed Martin.

1745419668305.png


"The established flying-wing layout aircraft model is based on the ICE verification aircraft proposed by Lockheed Martin [19]. This aircraft adopts a single-engine vector configuration, featuring a flying-wing design with high sweep angles and a tailless layout. It is primarily designed for air-to-air and air-to-ground attack missions. This configuration offers excellent stealth and supersonic performance, as illustrated in Figure 1. Its key parameters are listed in Table 1"

The paper is mainly about the Landing Control.
 
Top