that doesn't even make sense. I stated what Inst is saying certain thing and your reply is it is a wrong assumption?...... interesting.
I do not care who state what. If it is wrong, I will say so.
so you are saying that aircraft designers don't design the nose with the type of radar they would like to fit in mind?.... interesting.
No...They do not. At best, the military requirement of as capable a radar system as possible, such as the F-14 for fleet defense, will compel the design team to place antenna size as high consideration, but aerodynamics necessities override all.
You apparently don't speack any form of English or completely lack comprehension. I did not state definitively that J-10B is using AESA radar or PESA radar.
I said that if the following two statements are true:
1) CAC designed J-10B with AESA in mind
2) and the most optimal shape of the AESA radar is not circular.
I do not know and really do not care where you got the highlighted notion, or that you may perceive it to be true, but that is simply not true. It does not take much search to find that the F-35's AESA antenna is not elliptical =>
Then the following holds
They would design a fighter in J-10B with a non circular nose.
In no where there did I say 1 or 2 is true. So, either you are too busy trying to shot me down to read that or you have no comprehension of English.
This is obviously said in response to Inst who thinks the reason that J-10B's antenna were shaped non-circular due to the shape of J-10B's nose. He failed to see that they designed J-10B's nose non-circular in the first place possibly due to what kind of radar they had in mind.
Possibly...??? Again...Am getting the impression that people believe that antenna shape is dictated by antenna type. Regardless of who believe what, here is the truth...
Instead of designing a single complex antenna shape, the array uses a group of much simpler antenna shapes, and combines their individual signals together. In the fashion, all the mainlobes are added together, and if this is done correctly, a much tighter single mainlobe is produced.
An 'array' is technically speaking a complex arrangement of individual transmitters/receivers, even if each antenna in this complex arrangement is a classical concave dish. In this old and proven design, the wave superposition principle applied then as it is today. The main lobes of these individual antennas are -- in principle -- no different than the main lobes of individual T/R elements in an ESA antenna. The main advantage of modern day T/R elements is miniaturization.
In an ESA system, the antenna is
NOT the array. The antenna contain or 'hold' the array.
In the above (simplified) example...
(a) has the entire array produced a single very focused, or 'boresight', beam in azimuth and elevation. Ideal for closed in combat.
(b) has two independent 'flat' or 'thinned' arrays that are ideal for volume search in azimuth and elevation.
(c) has nine beams from one array. Two independent beams (black verticals) for elevation search, one narrow in azimuth, and six subarrays that can used for many things from target focus to communication.
(d) has six independent beams where each is focused on azimuth and elevation. Ideal for multiple targets in closed in combat.
A 'round' antenna would offer the greatest flexibility in subarray partitioning and choreography over an elliptical one. However, certain mission statements may compel an elliptical main array. But for a 'round' antenna, the subarray partitioning and choreography software will be able to create several beams of the same focus intensity, beam shape, and beam width for the techniques of time and spatial interleaving.
Time interleaving is useful for high target approach estimation at long distances. Several beams at slightly different freqs but focused on the same target will offer the greatest accuracy in vital target characteristics: altitude, speed, heading and aspect angle. Spatial interleaving is useful when several beams of the same focus intensity but at different freqs are aimed at multiple targets in closed-in combat.
Here is the main problem with exploiting the wave superposition principle for an array, be it the modern solid state T/R elements or small concave dishes...Beamwidth is
NOT from element count but from final array physical length. In other words, we can have the same number of T/R elements in two arrays but with different spacings between T/R elements for them. The sharpest beamwidth will be the array whose T/R element spacings approaches the critical quarter wavelength gap between elements. Remember...Both arrays (or subarrays) have the same T/R element count for each.
So if we go back to the subarray graphical illustration above...
If the mission statement is volume search, then (b) would be ideal for subarray partitioning and an elliptical main array would be appropriate. The two beams would be quite 'fan' shaped, one for volume azimuth and one for volume elevation.
If the mission statement is for combat in as diverse situations as possible, then we want either (c) or (d) subarray paritioning but with a 'round' main array so we can give the several individual beams equal T/R element count to give us better response ability for time/spatial interleaving of targets.
There is a second serious problem with an array, be it of modern solid state T/R elements or of the older design of complex arrangement of small concave dishes, that has to do with beam steering where the main beam gets wider as the sweep angle departs from 'straight on' and how different shapes of main arrays are appropriate for different situations but that is a different can of worms.