Originally posted by JB42
What about drag from ord racks? I was told (because i never did the testing myself) that there were some changes in the 190s and how they performed with/without ord hardpoints.
There is a measurable loss of speed when using bomb racks in the 190 aircraft, about 5 to 6 mph as far as I can tell.
All flight data commonly published for the P-51D includes the wing pylons. These were OEM, not added in the field and not something generally removed.
If you research the P-47, you will find that the P-47D-25-RE was delivered with pylons. These resulted in a 6 to 8 mph loss in speed. They were, however, easily removed. A P-47D-23-RE, minus the wing pylons, pulled 434.6 mph at best altitude. With the pylons, speed fell to 427.3 mph.
As we are about to receive the P-47N (we don't know if it will be a -1, -5, -15 or -25 model) and this was fitted with OEM pylons as well. With the pylons, speed is as follows from the testing of two production aircraft at Eglin Field.
P-47N-1-RE: All tests flown with full internal fuel at takeoff.
Time to Climb: 10.4 minutes to 25,000 feet.
Time to Climb: 6.2 minutes to 15,000 feet.
High Speed at WEP power (2,800 hp) 364 mph @ sea level.
High Speed at MIL power (2,100 hp) 332 mph @ sea level.
High Speed at MIL power (2,100 hp): 345 mph @ 5,000 feet.
High Speed at WEP power (2,800 hp): 378 mph at 5,000 feet.
High Speed at MIL power (1,760 hp): 438 mph at 42,000 feet.
High Speed at WEP power (2,800 hp) 467 mph at 32,000 feet.
High Speed at WEP power (2,490 hp) 455 mph at 38,750 feet.
My regards,
Widewing