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In article ,
"Jim Atkins" writes: Aren't there severe weight problems involved with separate vertical and horizontal systems? Seems I recall things like Dornier's transport (Do 31?) with dedicated lift jets that could just barely transport the weight of the crew. There are, especially in teh case of lift-jet aircraft, like the Dornier, which had to haul around a bimnch of engines that were only used for a short time each flight, but it's not that much of a problem with something like the Rotodyne, or even the almost-contemporary Lockheed AH-56. In the case of those aircraft, the rotors still provide lift, but they're unpowered, acting as an Autogiro fotor, and a fair chunk of the lift is taken up by the fixed wings. I guess you'd lose a bit of hover performance becase of the extra wing area under the rotor, but that would also accur with a tiltrotor. I suspect that Vmax would not theoretically be as high, you'd still have to deal with stuff like rotor tip speeds and retreating blade stall, but it'd be a fair shot. For the Rotodyne, noise was a severe problem. (Engine selection wasn't - Fairey wanted to move to teh Tyne for any later developments) If the newsreel soundtracks of teh thing I've heard are accurate, it could only be described as that of a Huey carrying a large, running Steam Locomotive. Consider this - Rotodyne noise was considered objectionable during a time when acceptable noise included unsuppressed straight-jet 707s and the just-proposed Concorde. You gotta go some to beat them. -- Pete Stickney A strong conviction that something must be done is the parent of many bad measures. -- Daniel Webster |
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