Dawncaster
Airman 1st Class
- 110
- Dec 23, 2013
Below you can see a Hellcat hooked up to a catapult. Note the Fowler flap system which is more effective than the split trail flaps use on the Seafire. Perhaps such a device might have either slowed the Spitfire down on landing or allowed it to land at lower angle of attack and thereby enjoy better visibility.
To modify the Spitfire I would be inclined to move the cockpit forward by reducing fuel tank volume to 2/3rds and also move the cockpit up slightly to give a better over the nose visibility. I would replace the lost fuel volume in either a tank below or behind the pilot. I would add a fowler flap system and a robust undercarriage and shock absorbing oleos.
I would add a P-51D style spine to the vertical tail to improve lateral stability with the enlarged rudder of the Mk VII/VIII. Ideally a coaxial contra rotating prop would be developed to cancel out any of the effects of torque, P factor, gyroscopic precession etc.
View attachment 615292
The Hellcat did not have Fowler flap system, it was NACA slotted flap. The Corsair also had the NACA slotted flap system, it's efficiency for lift cofficient was better than Hellcat's. Corsair had a lower stall speed and landing speed than the Hellcat, in landing condition. Nevertheless, for early F4U-1, it was found that large, effective and low positioned flaps had a negative impact on landing performance due to interference with the deck.
The Corsair's landing performance gradually improved, and the F4U-1D(FG-1D) was considered to have equivalent or even better landing performance than the F6F-5 in several evaluations and reports. Although there was also evaluation that the Hellcat had better all-around carrier characteristics.
It is possible that powerful flap system will not provide better landing performance always.