If thats true, and im not trying to argue here. Why did they strip every gun, ammo belt, metal plate and anything else that wasnt bolted down when they launched B-25's for the Doolittle raid? I appreciate they had limited distance to take off, ie: a carrier deck, but they also had limited fuel range too. And why did the Germans remove rear gunners, metal plates, landing gear spats and even the jericho sirens just to exchange weight for speed on the already slow Ju-87. And B-17 G's had nose mounted turrets. Surely that would be a clear aerodynamic mistake for a bomber that already had a slow cruising speed.
Before fighters like the Fw-190 & P-47/ Hawker Typhoon/Tempest, F4U, designers were of the opinion radial engines were never going to be better or faster than inlines, because of the drag/large surface area. Even recon fighters were stripped of all guns and ammo in favour of speed...... To say the aspect of speed vs weight is irrelevant is just silly
OOOKAAY.
1, They did not strip every gun from the Doolittle raiders.
Yes they had to take off from the carrier deck and according to one source this is the fuel load.
"the retractable ventral turret was removed, saving about 600 pounds of weight. More fuel was added to the plane, bringing the total fuel load to 1141 gallons--646 gallons in the wing tanks, 225 gallons in the bomb bay tank, 160 gallons in a collapsable tank carried in the crawlspace above the bomb bay, 160 gallons in the ventral turret space, and ten 5-gallon cans for refills." They
traded weight for fuel, not improved speed/performance by getting rid of weight.
2. I don't know about the JU-87 but is like putting lipstick on a pig. Were they improving speed? (and ditching the landing gear spats for naked landing gear is going to cost performance, not add to it.) Are you sure they weren't trying to carry a heavier than normal load?
3. Please compare speeds of a B-17G to a B-17F (without the front turret) the turret did cost some performance due to the increase in drag, the increase in weight ona B-17 is negligible.
4, I have no idea why you are bringing in the radial vs inline argument when the dispute is about weight vs speed.
5. Recon fighters were often stripped of guns (but not always) in order to fit either extra fuel or the cameras or to keep the CG in place with the change of equipment. Spitfires used the entire leading edge of the wing for fuel tanks. They traded armament weight for fuel weight. P-38s had up to five cameras in the nose and room and cg considerations dictated the removal of the guns.
A Merlin P-51 was 3 mph faster clean after it had burned off 1000lbs of fuel than when it was fully loaded but clean. Granted wing lift goes up with the square of the speed so a very fast plane is less bothered by weight increase than a slower plane.
Adding 15-20mph of cruise speed ( a liberal estimate) is not going to do much for survival against 350mph interceptors.
A lot of books about aircraft do confuse weight with loss of performance and ignore drag. Was it the weight of the Hispano cannon on the Spitfire that cost 5-6mph in speed or the projecting cannon barrels, the bumps on the wing to clear the ammunition feeds and the slot in the bottom of the wing for the cartridges to fall out of?
Was it the weight of the four cheek guns on a B-26 that had the manual saying the range was affected by 3% or the drag of the gun barrels and blisters?