Hybrid Airplanes developed by Boeing, page 1
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ATS Members have flagged this thread 2 times


reply posted on 2-8-2010 @ 06:02 PM by gagol
reply to post by stirling



I don't think so, it's more about turbine efficiency. But I am in no way an engineer.

Do we have an aeronautical engineer in the room?



reply posted on 2-8-2010 @ 06:27 PM by gagol
reply to post by oniongrass



Thank you very much oniongrass, that cleared things up a lot in my little marketer's head. Maybe I should take some of those free classes from MIT.


reply posted on 2-8-2010 @ 06:33 PM by oniongrass
reply to post by aspx



Calculate the energy used condensing the air to water, and extracting hydrogen from water. Then see if you get enough energy back in the remainder of your process to overcome that, plus lift the massive machinery needed to do all that.


reply posted on 2-8-2010 @ 06:58 PM by aspx
reply to post by oniongrass



yes i'm aware of that " condensing the air to water " its not big of a problem because 90% of the flow is just fresh air, the 10% is like a mini bomb implosion inside the engine, im thinking just to ride the air, like a tornado and have very strong magnetic fields compress hydrogen with incoming air. thus we only need little energy to create a powerful flow, similar to scram jet technology i would like to believe


reply posted on 2-8-2010 @ 07:37 PM by 4nsicphd
Originally posted by aspx
reply to
post by oniongrass



yes i'm aware of that " condensing the air to water " its not big of a problem because 90% of the flow is just fresh air, the 10% is like a mini bomb implosion inside the engine, im thinking just to ride the air, like a tornado and have very strong magnetic fields compress hydrogen with incoming air. thus we only need little energy to create a powerful flow, similar to scram jet technology i would like to believe


And where does that 10% come from? Even at 86 deg F, you get about 3% water vapor. When you get to the flight levels where drag allows transonic/supersonic flight, the water vapor density asymptotically approaches 0. And can I ask how you would get thrust from an "implosion"?
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