90% analogy is perhaps applicable while comparing present day JF-17 and F-16 but remaining listed aircrafts does not fall in the same league as present day F-16 i.e. blk52.
When hardware performance, such as rate of turn, sustainable g or thrust to weight ratio, between competing aircrafts begin to fall within %10 of each other, human factors such as training, experience, skill level and raw talent will have more influence on the outcome when the aircrafts are matched against each other. Note that US adversary air training uses technologically inferior aircrafts, such as the A-4 or the F-5, and routinely the adversary air pilots either outright defeat their opponents or made it very difficult for their opponents to use any hardware advantages in a fight. US Navy Top Gun instructors usually have far more flight hours and were among the top pilots at sea before their duties as adversary air trainers. I worked on a few US Navy F-16N and those F-16s were old A and C models and these pilots still gave their opponents good beatings.
Outside of this %10 margin and numerical superiority will be needed to anticipate and counter advantages created by the superior hardware. For example -- Fighters are g-limited by fuel load and weapons stores, the latter are external and centrifugal forces can do severe structural damages if the limiters are disabled or ignored. The F-16 is g-limited only by external stores and can sustain 9g turns with a full fuel load. It does not mean the aircraft will exceed that human safety figure of 9g with less fuel load. But what it does mean is that the air force that fly the F-16 can afford to base closer to the front line to take maximum advantage of this performance level to have increased time over the battlefield, ground or air, to penetrate deeper into enemy territory, again it is either ground or air, and if there is an aerial combat along the way, the F-16 will have enough fuel to use afterburners as often as he needed without worrying too much about fuel. The fighter that is outside of this %10 margin that goes up against the F-16 will need companions to try to anticipate the F-16's superior maneuverability to bring the F-16 down.
Next question is what specs do we require to intercept an aircraft as able as F-16 blk52 or F-16 it self!
Specs? The above F-16's fuel load example is only one of many criterias and I am going to expand on fuel a little to give you a sample of this complex issue.
Weapons and fuel are 'consumables', the radar computer is not a 'consumable' item, it is vital to aircraft operations. Weapons and fuel contribute to the aircraft's overall mass and can vary from day to day, making the aircraft's overall mass also a variable, so the goal is 'mass centralization' as mass distribution have a direct relationship to maneuverability. Fuel is unique in that as a liquid, its mass can move inside a container, aka 'sloshing', and the effect is well known from auto racing to boats to space...
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20090022238_2009022184.pdf
Predicting the effect of fuel slosh on the attitude control system of a spacecraft or launch vehicle is a very important and challenging task. Whether the spacecraft is spinning or moving laterally, the dynamic effect of the fuel slosh helps determine whether the spacecraft will remain on its intended trajectory. Three categories of slosh can be caused by launch vehicle or spacecraft maneuvers when the fuel is in the presence of an acceleration field. These are bulk-fluid motion, subsurface wave motion (currents), and free-surface slosh.
Basic physics tells us there is no such thing as 'decceleration', only 'acceleration' in the opposite direction and every time an aircraft make a maneuver like the famous split-S, there are 'acceleration fields' everywhere.
So to minimize the effect of fuel and its variable mass, an efficient fuel management scheme must be installed. Engine feed from the main fuselage tanks, but at the same time fuel from the wings are transfered inward into the fuselage tanks, keeping them full. If there are any external wing tanks hanging off pylons, their fuel is transferred up into the internal wing tanks, which then continue to be transferred into the fuselage tanks. Remember, we want to minimize centrifugal effects on mass that is furthest from the main body. Airliners have a different fuel management scheme where wing fuel remain there to maintain rigidity and stability for passenger comfort but that is another issue. For the F-16, how its fuel tanks are designed along with its efficient fuel management scheme contribute to its ability to sustain 9g turns while its fuselage tanks are full. In the real world, nothing is perfect so every fuel storage and management system will always be less than 1. A poorly designed fuel storage system will degrade or even negate any efficiency provided by the fuel transfer system, dragging the entire fuel system further away from 1. Management of 'consumables' will make or break a fighter.
In a typical combat scenario, an F-16 can take-off with a centerline external fuel tank, a 'consumable' item. On its wings will be bombs and missiles, more 'consumables' items. Over the target area, the centerline fuel tank will be empty but the tank itself will be retained. Then bombs are delivered. As the fighter attempts to return home, he is set upon by the opposing air force. He discard the centerline fuel tank to reduce mass. Now he is 'clean' with only missiles whose mass contribute minimal centrifugal effects in a turn. He is also most likely with full or near full internal fuel available for the coming aerial combat. If the opposing fighter have fuel related g-limiter while the F-16 does not, then fuel will be considered a negative factor against the opposing fighter. The F-16 will be able to out maneuver and out accelerate his opponent. The opposing fighter can make up for this deficiency with other factors such as two engines, or a more powerful radar, or along with the more powerful radar are longer distance missiles...etc...etc...But all these other factors cannot fall outside that %10 margin of performance comparability. The more any or all of these other factors fall outside of this %10 margin, the less pilot training, experience, skill and raw talent are able to compensate. I have tools in my garage but even a master mechanic is limited with my tools versus what he can accomplish with his professionally equipped shop.
The base F-16A model is still the standard for small and multi-role fighters in terms of performance. Any evolution, aka lettered (C/D) designations or 'blocks' of models, are essentially add-ons that increased the lethality of this base model. For example -- Changing to a higher output wattage radar or changing the flight control computer from analog to digital also does not affect the g-load capability of the airframe. These changes are described as 'C' or 'H' or whatever letter we want to use. So the answer to your question is mixed for this complex issue. If the JF-17 has an all digital avionics system but is g-limited due to varying fuel load, meaning sustainable turn rate is inverse to internal fuel load, then in a turning fight, the odds of losing to an all analog F-16A is good. Notice I said 'odds' as nothing but death and taxes are guaranteed. But if the JF-17 has a more powerful radar and longer distance missile to match, then how superior is the F-16A in a turn is largely irrelevant. Against later F-16 blocks, we have to examine the individual performance criterias, do some analysis and make an educated guess as how capable a JF-17 pilot could be, not will be, against his opponent.
Clear as mud?
JF-17 together with support of AWACS and ground based radars and defence system have more chance to tackel invading a/c. of even superior specs.
Vietnam is really not comparable to PAF armed with JF-17.
PAF have always emerged as winner in air battles with airforces far superior in tech and numbers. Strategy and utilization of available resources also counts, recently indian su-30 were locked by F-16A which is inferior to JF-17.
We expect JF-17 blk.II to be more stealthy, having better radar and engine.
Hence listed a/c can never beat PAF armed with 250 JF-17.
I hope you will abandon this tendency to make blanket statement after the sample explanation above.