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In article om,
wrote: When tested by the USN it was found that the Corsair was not suitable for use on carriers: 1 Long nose obscured sight of the deck 2 oil leaks over cockpit glass 3 undercarriage oleos would bottom out and bounce the aircraft of the landing wire 4 Abrupt stall. The royal Navy overcame 1 via a curved semi-circular approach and 2 by wiring the cowling shut over the windows. How were all of the other problems solved to allow carrier opperations? In the Corsair I the solution to 3. and 4. was to "be more careful landing". Corsair II had modified valving in the oelos, still needed care around the stall. Above is partially from Norman Hanson's "Carrier Pilot", partially directly from Norman himself (years ago). -- Andy Breen ~ Not speaking on behalf of the University of Wales, Aberystwyth Feng Shui: an ancient oriental art for extracting money from the gullible (Martin Sinclair) |
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On Sep 30, 2:24 am, Orval Fairbairn wrote:
In article , (Andrew Robert Breen) wrote: In article om, wrote: When tested by the USN it was found that the Corsair was not suitable for use on carriers: 1 Long nose obscured sight of the deck 2 oil leaks over cockpit glass 3 undercarriage oleos would bottom out and bounce the aircraft of the landing wire 4 Abrupt stall. The royal Navy overcame 1 via a curved semi-circular approach and 2 by wiring the cowling shut over the windows. How were all of the other problems solved to allow carrier opperations? In the Corsair I the solution to 3. and 4. was to "be more careful landing". Corsair II had modified valving in the oelos, still needed care around the stall. Above is partially from Norman Hanson's "Carrier Pilot", partially directly from Norman himself (years ago). They also lengthened the tailwheel oleo strut, so the "at rest" attitude of the aircraft approximated the landing attitude. An extended tail yoke was something that incidentally also belatedly solved the landing and takeoff problems of late model Me 109s. (Some Me 109G-10 and all Me 109K). Near its three point attitude the circulation caused by the propeller prop caused one wing to stall before the other. An extended yoke also increases ground visibility. A contra rotating prop probably would also have helped solve the problem as well as eliminate gyroscopic precession which also tends to otherwise cause a swing on takeoff. |
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On Sep 30, 12:19 am, (Andrew Robert Breen) wrote:
In article om, wrote: When tested by the USN it was found that the Corsair was not suitable for use on carriers: 1 Long nose obscured sight of the deck 2 oil leaks over cockpit glass 3 undercarriage oleos would bottom out and bounce the aircraft of the landing wire 4 Abrupt stall. The royal Navy overcame 1 via a curved semi-circular approach and 2 by wiring the cowling shut over the windows. How were all of the other problems solved to allow carrier opperations? In the Corsair I the solution to 3. and 4. was to "be more careful landing". Corsair II had modified valving in the oelos Propably a tapering rod that closed of the oriface through which the oleo oil flowed as the strut compressed. This would then tend to absorb the impact energy of landing and convert it into turbulent oil and heat instead of simply storing it and then releasing it. -- Andy Breen ~ Not speaking on behalf of the University of Wales, Aberystwyth Feng Shui: an ancient oriental art for extracting money from the gullible (Martin Sinclair) |
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