There seems to be a bit of confusion here.
The Defiant was designed as a two seat turret fighter and actually had a slightly smaller wing than the Hurricane (250sq ft). It also weighed around 1500lbs more but only around 800lbs of this was the actual turret, guns ammo and gunner so just wanking the turret out and plating over the opening still leaves the plane hundreds of pounds heavier. Without going back and redoing the stress calculations and redesigning structural components and even skin thickness that weight is not going to magically disappear.
The Battle was a
three seat light strategic bomber. It carried twice the payload of a Hart bomber twice as far. It was designed to get around a possible treaty restriction on the size/weight of bombers that never was implemented. It is a large single engine plane (422sq ft wing) , The Fulmar was based on a smaller two seat dive bomber derivative of the Battle that carried 1/2 the bomb load about 1/2 as far. The Fulmar had 8 feet less wingspan and a shorter/skinner fuselage and a 342sq ft wing.
Trying to
squish things around in these rather different airframes to try to do each others jobs is not really going to end well. That is give you a really useful airplane instead of one that fills a slot on paper and takes up hanger/apron space.
A lot depends
when you try to use the soft clay to squeeze the planes into different roles. For instance radios changed fairly quickly in the late 30s and first few years of the 40s. SOme accounts cali that the Defiant didn't use the same radios as the Hurricanes and Spitfires and could not communicate with them. Long range radios (as needed by bombers and planes flying over water) often needed a dedicated operator but just a few years later newer radios that were easier to operate and longer ranged did away with the need for the 2nd crew man.
Trying to adapt land planes to carriers is also a can of worms.
Granted this is the HMS Argus but non-folding wings presented a lot of problems on carriers.
take-off speeds and landing speeds were also critical. A 10% increase in landing speed (from say 70mph to 77mph) is actually 21% higher in the energy the arresting system has to deal with. On a moving carrier it is worse. Assuming the carrier is moving at 20mph the difference in relative energy of the 70mph airplane and the 77mph airplane is just under 30%.
The Defiant had a higher landing speed than the Hurricane or Spitfire, adding another fighter to the FAA that didn't have folding wings (the Fulmar did) doesn't solve any problems for the FAA.
The whole P.94 story seems to have a few holes. The Defiant was about 20mph slower than a Hurricane using the same engine, The P. 94 was supposed to be 20mph faster by dropping the turret? The 360mph speed for the P. 94 was an estimate based off the trials of the prototype Defiant. However the Defiant II with Merlin XX engine didn't quite meet the estimates for it. How much of that was due to the flat black paint and radar aerials, how much was due to a high drag radiator (larger than the radiator for the Merlin III) or for other reasons I don't know but getting 40mph just for dropping the turret seems a bit much. (it also takes no account of sticking guns in the wings?)