What was the best post-WW II fighter ?

in 1 vs 1 situation which one will come out the best , second , last ? , which one better at low/ medium / high altitude
P-51H

P-51H Mustang
Data from The Great Book of Fighters[124]
General characteristics
Crew: 1
Length: 33 ft 4 in (10.16 m)
Wingspan: 37 ft 0 in (11.28 m)
Height: 11 ft 1 in (3.38 m)
Wing area: 235 ft² (21.83 m²)
Empty weight: 7,040 lb (3,195 kg)
Loaded weight: 9,500 lb (4,310 kg)
Max takeoff weight: 11,500 lb (5,215 kg)
Powerplant: 1× Packard V-1650-9 liquid-cooled supercharged V-12, 1,490 hp (1,111 kW) at 3,000 rpm, 2,220 hp (1,655 kW) at WEP[128]
Performance
Maximum speed: 487 mph (784 km/h) at 25,000 ft (7,600 m)
Range: 1,160 mi (1,865 km) with external tanks
Service ceiling: 41,600 ft (12,700 m)
Rate of climb: 3,300 ft/min (16.8 m/s)
Wing loading: 40.4 lb/ft² (197.4 kg/m²)
Power/mass: 0.23 hp/lb (385 W/kg)

F4u-4

General characteristics
Crew: 1 pilot
Length: 33 ft 8 in (10.2 m)
Wingspan: 41 ft 0 in (12.5 m)
WS Folded: 17 ft 0.5 in (5.2 m)
Height: 14 ft 9 in (4.50 m)
Empty weight: 9,205 lb (4,174 kg)
Loaded weight: 12,405 lb (5,626 kg)
Powerplant: 1 × Pratt & Whitney R-2800-18W radial engine, 2,325 hp (1,710 kW)
Performance
Maximum speed: 453 mph (395 kn, 731 km/h)
Range: 897 mi (602 nmi (1,115 km))
Service ceiling: 41,500ft (12,649 m)
Rate of climb: 3,870ft/min (19.7 m/s)

Focke-Wulf Ta 152 H-1

Crew: One
Length: 10.82 m (35 ft 5 63/64 in)
Wingspan: 14.44 m (47 ft 4 1/2 in)
Height: 3,36 m (13 ft 1in)
Wing area: 23.5 m² (253 ft²)
Empty weight: 4,031 kg (8,640 lb)
Loaded weight: 4,727 kg (10,470 lb)
Max. takeoff weight: 5,217 kg (11,501 lbs)
Powerplant: 1 × Jumo 213E liquid-cooled inverted V-12, 1,287 kW (1,750 PS; 2,050 PS with MW-50)
Performance
Maximum speed: 759 km/h at 12,500 m using GM-1 boost (472 mph at 41,000 ft using GM-1 boost)
Range: 2,000 km (1,240 mi)
Service ceiling: 15,100 m using GM-1 boost (49,540 ft using GM-1 boost)
Rate of climb: 20 m/s to 25.4 m/s (3,937 ft/min at maximum weight of 5,217 kg to ~5,000+ ft/min at 4,727 kg)
Wing loading: 196.8 kg/m² (41.38 lb/ft²)
Power/mass: 0.276 kW/kg (0.167 hp/lb)

Nakajima Ki-84 Hayate

Crew: One
Length: 9.92 m (32 ft 7 in)
Wingspan: 11.238 m (36 ft 11 in)
Height: 3.385 m (11 ft 1 in)
Wing area: 21 m² (226.041 ft²)
Empty weight: 2,660 kg (5,864 lb)
Loaded weight: 3,601.5 kg (7,940 lb)
Max. takeoff weight: 4,170 kg (9,194 lb)
Powerplant: 1 × Nakajima Ha-45-21 Homare 18-cylinder radial engine, 1,522 kW at SL, 1360 kW at 17,900 ft (1,970 hp at SL, 1850 hp at 17,900 ft)
Performance
Never exceed speed: 800 km/h (496 mph)
Maximum speed: 686 km/h (426 mph) at 7,020 m (23,000 ft)
Range: 2,168 km (1,347 mi)
Service ceiling: 11,826.24 m (38,800 ft)
Rate of climb: 21.84 m/s at SL, 18.29 m/s at 3050 meters (4300 ft/min at SL, 3600 ft/min at 10,000 ft)
Wing loading: 171.47 kg/m² (35.1 lb/ft²)
Power/mass: 1.8 kg/hp (4 lb/hp)

F8F-2 Bearcat

Length: 28 ft 3 in (8.61 m)
Wingspan: 35 ft 10 in (10.92 m)
Height: 13 ft 10 in (4.21 m)
Empty weight: 7,650 lb (3,207 kg)
Loaded weight: 10,200 lb (4,627 kg)
Max. takeoff weight: 13,460 lb (6,105 kg)
Powerplant: 1 × Pratt & Whitney R-2800-30W two-row radial engine, 2,250 hp (1,678 kW)
Performance
Maximum speed: 455 mph (405 kn, 730 km/h)
Range: 1,105 mi (1,778 km)
Service ceiling: 40,800 ft (12,436 m)
Rate of climb: 4,465 ft/min (23.2 m/s)
Power/mass: 0.22 hp/lb (360 W/kg)

Spiteful XIV

General characteristics
Crew: One
Length: 32 ft 11 in (10.03 m)
Wingspan: 35 ft 0 in (10.67 m)
Height: 13 ft 5 in (4.09 m)
Wing area: 210 ft² (19.5 m²)
Empty weight: 7,350 lb (3,331 kg)
Max. takeoff weight: 9,950 lb (4,523 kg)
Powerplant: 1 × Rolls-Royce Griffon 69 V-12 engine, 2,375 hp (1,772 kW)
Performance
Maximum speed: 483 mph (420 knots, 778 km/h) at 21,000 ft (6,400 m)
Range: 564 mi (490 nmi, 908 km)
Service ceiling: 42,000 ft (12,800 m)
Rate of climb: 4,890 ft/min (24.8 m/s)

me-262

Crew: 1
Length: 10.60 m (34 ft 9 in)
Wingspan: 12.60 m (41 ft 6 in)
Height: 3.50 m (11 ft 6 in)
Wing area: 21.7 m² (234 ft²)
Empty weight: 3,795 kg[88] (8,366 lb)
Loaded weight: 6,473 kg[88] (14,272 lb)
Max. takeoff weight: 7,130 kg[88] (15,720 lb)
Powerplant: 2 × Junkers Jumo 004 B-1 turbojets, 8.8 kN (1,980 lbf) each
Aspect ratio: 7.32
Performance
Maximum speed: 900 km/h (559 mph)
Range: 1,050 km (652 mi)
Service ceiling: 11,450 m (37,565 ft)
Rate of climb: 1,200 m/min (At max weight of 7,130 kg) (3,900 ft/min)
Thrust/weight: 0.28

btw why can’t i find the thrust-weight ratio of piston fighter ?