Let say for a moment, we ignore boring limitation like production cost, maintenance issue, complexity, stealth characteristic. What would be the best aerodynamic configuration for a fighter jet? and why ?. I'm not talking about the
Tandem configuration with both rear horizontal tail and canard
Advantage:
Can generate huge amount of lift at low speed and low AoA, yet still allow your aircraft reaching high speed. Arguably the only other configuration along with VG that allow heavy fighter to land on carrier
Better lift generation for high AoA maneuver
Long arm canard:
Advantages: low drag, especially at supersonic speed, good moment for turning at high speed, high altitude
Variable swept wing:
Advantage: arguably the only kind of wing that can give optimum L/D ratio at all speed range. It can give the highest amount of lift at low speed, low AoA and lowest amount of drag at high speed
VG wing give lowest landing speed and highest top speed at the same time
Close coupled canard:
Advantages: low drag especially at supersonic speed. Can generate a lot of lift for turning, good high AoA characteristic
Tandem configuration with both rear horizontal tail and canard
Advantage:
Can generate huge amount of lift at low speed and low AoA, yet still allow your aircraft reaching high speed. Arguably the only other configuration along with VG that allow heavy fighter to land on carrier
Better lift generation for high AoA maneuver

Long arm canard:
Advantages: low drag, especially at supersonic speed, good moment for turning at high speed, high altitude

Variable swept wing:
Advantage: arguably the only kind of wing that can give optimum L/D ratio at all speed range. It can give the highest amount of lift at low speed, low AoA and lowest amount of drag at high speed
VG wing give lowest landing speed and highest top speed at the same time

Close coupled canard:
Advantages: low drag especially at supersonic speed. Can generate a lot of lift for turning, good high AoA characteristic
