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The 1st time the rack was installed, it was under the centreline.
The early Corsairs have had no racks what so ever. The 1st time the rack was installed, it was under the centreline. Later models got two racks under the inner wing portion, the centreline rack being removed. Post war the centreline rack was installed.
The prototype Corsair have had bomb bays in the wings for small anti-aircraft bombs.
Because they wouldn't hit the propeller. Both the the USAAF and the USN established this independently, the USAAF using 'vertical' dives with a P-47. I'd have to look up which aircraft the USN used, but the results were discussed at the Patuxent River fighter conference and I posted the relevant section in another thread sometime ago.
'Vertical' dives, at least in USAAF parlance, seem to refer to any dive at an angle of 70 degrees or more...not necessarily literally vertical.
Cheers
Steve
The bomb definetely accelerates faster than the aircraft, .
Only the force of gravity could act to accelerate the bomb. Whether it will accelerate the bomb or whether the bomb will in fact decelerate once released depends on the forces opposing gravity, principally the drag of the bomb.
I have no idea how that works out for different scenarios, but knowing the terminal velocity at typical altitudes for the bomb(s) would be a good starting point.
Steve
OK. True vertical dive bomb scenario:
- Typical terminal velocities of the bombs I have have seen quoted is about 600mph.
- F4U limit speed with its gear extended is 250-260knots, or 300mph.
The bomb ejector was used on the AD Skyraider according to the Pilot's Handbook for AD-2/AD-3 and AD-4. Section 4-19 of AD-2/AD-3 pilot's handbook states:Essentially that the aircraft separates from and accelerates away from the bomb.
pp156/7 of my edition of the 'Report of Joint Fighter Conference'.
Commander Monroe:
"Our fighters are authorized to dive up to 85 degrees. Of course they have no displacing gear. Careful investigation down here shows absolutely no danger of the bomb hitting the propeller. At least the airplane and the bomb keep their relative pressures fore and aft, and the bomb drops away from the airplane, which was a great relief to everybody."
This agrees broadly with what the USAAF had also discovered.
Whether 'our fighters' includes the F4U I can't say for sure. The date of the conference was 16th - 23rd October 1944, so it had been in service for some time.
In the interest of balance, I have read somewhere (can't remember where) that Douglas were developing a bomb displacement system powered by a cartridge, and an automatic pull out system, both designed to throw a bomb clear of an aircraft propeller. I don't know which aircraft were involved, and as far as I know such a system never saw service. I would happily be corrected, US aircraft are not really my forte
Cheers
Steve
The bomb ejector provided with the fuselage bomb rack is designed to displace the bomb away from the airplane sufficiently to clear the propeller in steep dives and operates by means of a bomb ejector cartridge.
,
Better recalculate.
F4U, specified, limited the dive angle to 60 degrees, see post #8.And USN fighters, unspecified, were cleared to dive at 85 degrees, close to a true vertical, with no danger of the bomb hitting the propeller.
F4U, specified, limited the dive angle to 60 degrees, see post #8.
And USN fighters, unspecified, were cleared to dive at 85 degrees, close to a true vertical, with no danger of the bomb hitting the propeller.
Same for the P47.
There are complicated aerodynamic forces at work.