Smokey said:
If it is at a relatively high altitude above the p51, then yes
P-51 needed to be a lot faster and higher to fight against a P-38, as at least one P-51 driver told his Nephew.
Acording to many pilots that flew both they prefered the P-38 dogfighting and Stienhoff cited the "Clear superority of the Lightning in speed and maneuverability" for the loss of air superority over Sardinia.
Art Heiden prefers the P-38L with comments like - theres nothing the doomed German pilot can do to get away from the P-38L or "The Mustang was a delight to fly, easier to maintain, chealer to build and train pilots for and had long legs. In those respects you could say it was better, but it could not do anything better than a P-38J-25 or L".
A twin has some advantages and depending of design intent/efficency disadvantages. The point made above about propellar clearance is true and it could have disastours cosequenses on the handling of a twin engined fighter.
Advantages (counter rotating props/jet engines)
1. Redundancy
2. Load capacity for fuel and ordanence
3. Stability for aiming and flying
4. Great stall characteristics in all regimes
5. Engine/prop tourque Help during maneuvering
6. Tricycle gear are easier to mount (Reciprocating engines normaly mounted in front)
Dissadvantages
1. Complexity
a. Construction
b. Maintenance (though in the case of the P-38 engines overhaul rates on both Allisons were only about 25% greater than one Merlin and 30% greater than one 2800.
2. Fuel consumption (though the P-38 used 1,030gal for 2,600mi to a P-47Ns 1,165gal for 2,300mi)
3. Size (again the P-38 is only larger than a P-51/P47 from above)
I mention the P-38 for two reasons first I'm more familiar with it and second I think I paved the way and convinced those concerned that a twin engined fighter was not only viable but could be very competitive ans versatile.
wmaxt