wing loading is just a metric. The actual useful indicator that wing loading is attempting to correlate to is how much additional lift the airplane can generate by pulling higher angle of attack without causing drag to increase exponentially snd the airplane effectively stalling.
In real life, even in a fighter with big wings, the lift generated by the fuselage and air intake can account for more than half of the total lift generated by the fighter.
So take any comparison of wing loading as measure of sustained turn rate with a grain of salt.
That being said, a twin engine fighter like the Rafale and Eurofighter tend to deribe somewhat higher percentage of its total lift generated from its fuselage than single engine fighters such as F-16 and J-20. So if the wing loading of twin engine fighter as measured purely based on wing area is the same as that of a single engine fighter, the true aerodynamic lift loading of the entire aircraft is likely to be lower in the case of the twin engine aircraft.
So all else being the same, a twin engine fighter is likely to have somewhat higher sustained turn rate compared to a single engine fighter. This was one justification the TsAGI gave recommending to Mikoyan that the Mig-29 be a twin engine design. So in this one needs to give Eurofighter snd Rafale a slight handicap when comparing wing loading based on wing area.
conversely, all else being the same, a single engine fighter is likely to have less polar moment of inertia than a comparable twin engine fighter. it is would roll faster and this be more agile than the twin engine fighter.
In real life, even in a fighter with big wings, the lift generated by the fuselage and air intake can account for more than half of the total lift generated by the fighter.
So take any comparison of wing loading as measure of sustained turn rate with a grain of salt.
That being said, a twin engine fighter like the Rafale and Eurofighter tend to deribe somewhat higher percentage of its total lift generated from its fuselage than single engine fighters such as F-16 and J-20. So if the wing loading of twin engine fighter as measured purely based on wing area is the same as that of a single engine fighter, the true aerodynamic lift loading of the entire aircraft is likely to be lower in the case of the twin engine aircraft.
So all else being the same, a twin engine fighter is likely to have somewhat higher sustained turn rate compared to a single engine fighter. This was one justification the TsAGI gave recommending to Mikoyan that the Mig-29 be a twin engine design. So in this one needs to give Eurofighter snd Rafale a slight handicap when comparing wing loading based on wing area.
conversely, all else being the same, a single engine fighter is likely to have less polar moment of inertia than a comparable twin engine fighter. it is would roll faster and this be more agile than the twin engine fighter.
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