Re: Could soundbarrier be broken with a prop plane ?
YB-49 case may be so but XB-42 did suffer yaw problems; http://en.wikipedia.org/wiki/XB-42_Mixmaster
One thing that bugs me is the long distance from the prop to the aerodynamical center in rod connected fan pushers. The gyro forces really do exist and lot more effective area thus needed in elevator rudder section.
What about situation where engine siezes..and stop propelling the thing ? again the ailerons have to compensate and are far from tha cause of the twist...this was a big problem in P-51D ( increase of power at low speeds caused bank to the left ).
I have to start believing you Red in this Bede-5b size matter...it has a lot of radiator and use of the tricycle retractable landing gear also takes room.
Why I think pushers will inevitably win is the less gas burning layout travelling at reasonably fast speed...evident also in XB-42. Jetmaster XB-43 with same frame wasn't much faster: http://en.wikipedia.org/wiki/XB-43_Jetmaster
Originally posted by Red
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One thing that bugs me is the long distance from the prop to the aerodynamical center in rod connected fan pushers. The gyro forces really do exist and lot more effective area thus needed in elevator rudder section.
What about situation where engine siezes..and stop propelling the thing ? again the ailerons have to compensate and are far from tha cause of the twist...this was a big problem in P-51D ( increase of power at low speeds caused bank to the left ).
I have to start believing you Red in this Bede-5b size matter...it has a lot of radiator and use of the tricycle retractable landing gear also takes room.
Why I think pushers will inevitably win is the less gas burning layout travelling at reasonably fast speed...evident also in XB-42. Jetmaster XB-43 with same frame wasn't much faster: http://en.wikipedia.org/wiki/XB-43_Jetmaster
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