davparlr
Senior Master Sergeant
Dave - as I noted to Jim, I know what the design philosopy was on both the D and the H as I posted to Jim.
Simply I believe the handbook reference is in error... but I do believe the two airframes are EQUIVALENT across the board as long as the load out of fuel and ammo are the same - simply because the H would be 400 pounds lighter across the load profile
The simple math would look like this..
at 8000 pounds at 12G, the B and D wing would be designed to fail with 96,000 pounds applied to each wing
at 8000 pounds at 11.5G the H wing would fail at 92,000 pounds
at 8400 pounds the D wing still fails at 96000 pounds - but the 'allowable G' at that weight is 96,000/8400 = 11.42 G Ultimate ------> same as the P-51H with same loadout but lower gross weight at 8000 pounds.
The difference in real life is negligible but I don't believe the P-51H was 10% 'stronger'.
Part of stripping the weight was better design (straight leading edge/no strake, smaller main gear, etc), and pasrt was resizing caps and stringers after several years of failure history to better balance the structural integrity... so they a.) took out some unneccesary redundancy and b.) lowered the design limit and design ultimate accordingly based on reduced weights.
Thanks for you excellent explaination!