Now imagine development continuing from April 1943 on based not on the J model, but rather on the K model. Four blade propellers would have become standard (owing to standardization of production), again improving performance.
For the most part, development of the P-38 really halted in 1943, other than detail work. Serious attempts to improve the airframe and the engines almost completely ceased. Time and resources were wasted on various "related" projects instead.
Of course, the biggest reason Lockheed couldn't halt production long enough to introduce the K model was that 1/2 the Burbank plant was building B-17 bombers, as much to replace losses due to unescorted bombing missions as any other reason. While Consolidated Vultee of Nashville TN struggled for 2-3 years to produce a paltry 113 P-38 fighters. Probably because Boeing was not happy with the idea of allowing Consolidated to build a Boeing aircraft.
If you read this :
http://www.ausairpower.net/P-38-Analysis.html you'll see that other detail improvements were not made for much the same reasons.
Those two articles were written by Widewing, and Dr Carlos Kopp, with help from two P-38 pilots, Captain Stan Richardson Jr., and Captain Arthur Heiden, both of whom I swapped hundreds of emails with. Of particular interest in Dr. Kopp's article is a statement about climb rate and combat radius with regard to combat effectiveness by Art Heiden. Now consider again the P-38K in that regard. Consider also the effect of the power and propeller efficiency on acceleration and the ability to retain speed and energy.
To steal a line from Rod Steiger, imagine if you will, the P-38L based not on the P-38J, but rather on the P-38K, as it should have been. And then consider what it would have meant if Lockheed Burbank were using both halves of the plant capacity to produce the P-38, instead of half the plant producing the B-17, which, in late 43 and all of 44 was as much bait for the fighters over Europe as it was anything else. What you'd end up with would be around 10K P-38L fighters with a top speed of around 450MPH at 26K feet, around 4K fpm sustained rate of climb, and a 20% combat radius cushion.