No, it is uniform RCS.
Declassified information at a glance:
http://www.airforcemag.com/MagazineArchive/PublishingImages/2019/May 2019/F-15.F-35_Vertical.v30.pdf
RCS reduction measures are numerous, and many of these measures are not thoroughly/properly elaborated in public domain (understandable). There is no such thing as a standard stealth design for every developer to emulate
but select-few rcs reduction PRINCIPLES are important considerations in theory. For instance, shaping should be done in the manner as to deflect radar waves in directions away from the emitter and high quality RAM coatings should be applied to the surface to minimize 'surface reflections' by turning the energy into heat.
Shaping might be 90% important and materials might be 10% important for rcs reduction in theory, but this isn't true in practice. Below is some revelation:
"The F-22's RCS was equated to that of a marble (−40 dBsm) during development, but is rumored to have beaten this figure. The F-35's RCS was originally equated to that of a golf ball (−30 dBsm), but more recently insiders have hinted its RCS might have beaten the F-22 with its superior modeling, stealthier intakes and advanced materials." - Aviation Week
Construction secrets HINTED.
F-35's airframe =
42% of composite fiber mat
F-22's airframe = 22% of composite fiber mat
F-16's airframe = 2% of composite fiber mat
Composite construction is essential to reduce 'mismatches and gaps' that create unwanted radar reflections off the aircraft's body and surfaces.
F-35's airframe also feature non-perpendicular corners to suppress 'surface reflections'. Lockeed Martin's revolutionary RAM coatings suppress 'surface reflections' even more.
An important consideration is to limit the number of edges an aircraft has, and to align the existing edges to a small number of directions; parts that stick up with a lot of edges need to be covered by a curved surface. F-35 have blended curves all around accordingly.
Once again, flat body structure is not necessary, might not be technically feasible based on the type of war-fighting capabilities expected from the finalized product, and neither it will make much difference all on its own. A developer need to factor-in various war-fighting technicalities in order to develop a very capable war-machine within a specified budget. Therefore, developer will have to look for additional ways to ensure VLO output, and this is why true VLO aircraft are very expensive and difficult to design on the whole.
Design of engine; exhaust structure; exhaust nozzles; avionics; and RAM coatings = every facet will make difference in the end.
Refer back to my revelations in post # 2410:
https://defence.pk/pdf/threads/sac-...-updates-debate.343466/page-161#post-11536231
All of it flew over your head, didn't it?
Chinese LO designs have significant shortcomings which trained eyes can easily notice and pinpoint. FC-31 prototype (31001) is an RC toy in comparison to F-35 in its current form (Block-3f). Provide technical evidence to the contrary, if you can.