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Greater lift for aircraft
"JaxAshby" wrote in
ink.net: Aircraft get greater lift just after takeoff if they leave their landing gear down. That's because the tires are still rotating from takeoff and they provide lift in the airstream via the Magnus effect. Betcha ole Bertie didn't know that. Betcha old Bertie has forgotten more about airplanes than you'll ever know, fjuckwit. Bertei |
Greater lift for aircraft
"JaxAshby" wrote in
ink.net: Aircraft get greater lift just after takeoff if they leave their landing gear down. That's because the tires are still rotating from takeoff and they provide lift in the airstream via the Magnus effect. Betcha ole Bertie didn't know that. Jax the Bunyip biter. Oh Jaxholio, while you're here, settle an argument. Who sent you running like the little girl you are, me, or the lusers in the froup? BTW, got any more pics of yourself? I lurved the ones you posted before! Bertie |
Greater lift for aircraft
Wassa matta Berts?
I betcha neva lurned the Magnus effect so ya culd neva furgit it in the furst place. In fact, yur a trade skool pilot dimwit! Bite me bunyip! Jax the one who barrel rolls the bunwipe "Bertie the Bunyip" wrote in message ... "JaxAshby" wrote in ink.net: Aircraft get greater lift just after takeoff if they leave their landing gear down. That's because the tires are still rotating from takeoff and they provide lift in the airstream via the Magnus effect. Betcha ole Bertie didn't know that. Jax the Bunyip biter. Oh Jaxholio, while you're here, settle an argument. Who sent you running like the little girl you are, me, or the lusers in the froup? BTW, got any more pics of yourself? I lurved the ones you posted before! Bertie |
Greater lift for aircraft
And yet you seem unable to answer his qeustion????
Regards Donal -- "Bertie the Bunyip" wrote in message ... Flying Tadpole wrote in : JaxAshby wrote: Aircraft get greater lift just after takeoff if they leave their landing gear down. That's because the tires are still rotating from takeoff and they provide lift in the airstream via the Magnus effect. Betcha ole Bertie didn't know that. Jax the Bunyip biter. Three sentences? All more or less coherent? Clearly a forged identity. could be. but the cluelessness certainly reeks of Jax Bertie |
Greater lift for aircraft
"Donal" wrote in
: And yet you seem unable to answer his qeustion???? What question? He made a statement which is almost correct, though limited in scope and insignificant to boot. Bertie Regards Donal -- "Bertie the Bunyip" wrote in message ... Flying Tadpole wrote in : JaxAshby wrote: Aircraft get greater lift just after takeoff if they leave their landing gear down. That's because the tires are still rotating from takeoff and they provide lift in the airstream via the Magnus effect. Betcha ole Bertie didn't know that. Jax the Bunyip biter. Three sentences? All more or less coherent? Clearly a forged identity. could be. but the cluelessness certainly reeks of Jax Bertie ------=_NextPart_000_0030_01C35F8D.303F7B40 !DOCTYPE HTML PUBLIC "-//W3C//DTD HTML 4.0 Transitional//EN" HTMLHEAD META http-equiv=Content-Type content="text/html; charset=iso-8859-1" META content="MSHTML 5.50.4134.600" name=GENERATOR STYLE/STYLE /HEAD BODY bgColor=#ffffff DIVFONT face=Arial size=2And yet you seem unable to answer his qeustion????/FONT/DIV DIVFONT face=Arial size=2/FONT /DIV DIVFONT face=Arial size=2/FONT /DIV DIVFONT face=Arial size=2Regards/FONT/DIV DIVFONT face=Arial size=2/FONT /DIV DIVFONT face=Arial size=2Donal/FONT/DIV DIVFONT face=Arial size=2-- /FONT/DIV DIV /DIV BLOCKQUOTE style="PADDING-RIGHT: 0px; PADDING-LEFT: 5px; MARGIN-LEFT: 5px; BORDER-LEFT: #000000 2px solid; MARGIN-RIGHT: 0px" DIV"Bertie the Bunyip" <A /A> wrote in message A . com"news:bh4nq0$do /A.../DIVFlying Tadpole <A "flyingtadp /A > wrote inBRA "news:3F3 5DCE2.65A90C97@hotm ail.com/A: BRBR> BR> BR> JaxAshby wrote:BR>> BR>> Aircraft get greater lift just after takeoff if they leave theirBR>> landing gear down. That's because the tires are still rotating fromBR>> takeoff and they provide lift in the airstream via the Magnus effect.BR>> Betcha ole Bertie didn't know that.BR>> BR>> Jax the Bunyip biter.BR> BR> Three sentences? All more or less coherent? Clearly a forgedBR> identity.BRBRcould be. BRBRbut the cluelessness certainly reeks of JaxBRBRBertie/BLOCKQUOTE/BODY/HTML ------=_NextPart_000_0030_01C35F8D.303F7B40-- |
Greater lift for aircraft
That makes no sense, according to that theory the wheel should lower the
amount of lift, seeing as the lower part of the wheel is going in the direction of the air. "Bertie the Bunyip" wrote in message ... "JaxAshby" wrote in ink.net: Aircraft get greater lift just after takeoff if they leave their landing gear down. That's because the tires are still rotating from takeoff and they provide lift in the airstream via the Magnus effect. Betcha ole Bertie didn't know that. Betcha old Bertie has forgotten more about airplanes than you'll ever know, fjuckwit. Bertei |
Greater lift for aircraft
"mbrookesn231" wrote in
le.rogers.com: That makes no sense, according to that theory the wheel should lower the amount of lift, seeing as the lower part of the wheel is going in the direction of the air. nope, he's right, It's the greater speed of the upper part of the wheel that would increase it but it's insignificant in any case. Bertie "Bertie the Bunyip" wrote in message ... "JaxAshby" wrote in ink.net: Aircraft get greater lift just after takeoff if they leave their landing gear down. That's because the tires are still rotating from takeoff and they provide lift in the airstream via the Magnus effect. Betcha ole Bertie didn't know that. Betcha old Bertie has forgotten more about airplanes than you'll ever know, fjuckwit. Bertei |
Greater lift for aircraft
Bertie the Bunyip wrote in message . ..
"mbrookesn231" wrote in le.rogers.com: That makes no sense, according to that theory the wheel should lower the amount of lift, seeing as the lower part of the wheel is going in the direction of the air. nope, he's right, It's the greater speed of the upper part of the wheel that would increase it but it's insignificant in any case. Bertie the amount of theoretical lift generated is negligible, whereas the drag generated from extended gear is not |
Greater lift for aircraft
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Greater lift for aircraft
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Greater lift for aircraft
"Bertie the Bunyip" wrote in message ws.com... (running with scissors) wrote in om: Bertie the Bunyip wrote in message . .. (running with scissors) wrote in om: Bertie the Bunyip wrote in message . .. "mbrookesn231" wrote in le.rogers.com: That makes no sense, according to that theory the wheel should lower the amount of lift, seeing as the lower part of the wheel is going in the direction of the air. nope, he's right, It's the greater speed of the upper part of the wheel that would increase it but it's insignificant in any case. Bertie the amount of theoretical lift generated is negligible, whereas the drag generated from extended gear is not Well, exactly. though on some aircraft the drag caused during retraction is considered worse than leaving it down in the event of an engine failure! Bertie true. Can't think of one off the top of my head, though! Bertie Any A/C that the gear rotates 90 degrees to stow would have greater drag during the "Rotate/Stow" sequence. Ralph Nesbitt Professional FD/CFR/ARFF Type |
Greater lift for aircraft
Ralph Nesbitt wrote:
Well, exactly. though on some aircraft the drag caused during retraction is considered worse than leaving it down in the event of an engine failure! Bertie true. Can't think of one off the top of my head, though! Any A/C that the gear rotates 90 degrees to stow would have greater drag during the "Rotate/Stow" sequence. Many aircraft have gear doors that open for retraction/extension, but are closed when the gear is locked in place, either up or down. In those aircraft, drag will be higher during the extension or retraction sequence, as an extra door is open and hanging in the breeze. Mike |
Greater lift for aircraft
"Ralph Nesbitt" wrote in
: "Bertie the Bunyip" wrote in message ws.com... (running with scissors) wrote in om: Bertie the Bunyip wrote in message . .. (running with scissors) wrote in om: Bertie the Bunyip wrote in message . .. "mbrookesn231" wrote in le.rogers.com: That makes no sense, according to that theory the wheel should lower the amount of lift, seeing as the lower part of the wheel is going in the direction of the air. nope, he's right, It's the greater speed of the upper part of the wheel that would increase it but it's insignificant in any case. Bertie the amount of theoretical lift generated is negligible, whereas the drag generated from extended gear is not Well, exactly. though on some aircraft the drag caused during retraction is considered worse than leaving it down in the event of an engine failure! Bertie true. Can't think of one off the top of my head, though! Bertie Any A/C that the gear rotates 90 degrees to stow would have greater drag during the "Rotate/Stow" sequence. Ralph Nesbitt Well, I ws thinking more of ther gear doors opeing and closing during the sequence. Bertie |
Greater lift for aircraft
Bertie the Bunyip wrote in message . ..
"Ralph Nesbitt" wrote in : "Bertie the Bunyip" wrote in message ws.com... (running with scissors) wrote in om: Bertie the Bunyip wrote in message . .. (running with scissors) wrote in om: Bertie the Bunyip wrote in message . .. "mbrookesn231" wrote in le.rogers.com: That makes no sense, according to that theory the wheel should lower the amount of lift, seeing as the lower part of the wheel is going in the direction of the air. nope, he's right, It's the greater speed of the upper part of the wheel that would increase it but it's insignificant in any case. Bertie the amount of theoretical lift generated is negligible, whereas the drag generated from extended gear is not Well, exactly. though on some aircraft the drag caused during retraction is considered worse than leaving it down in the event of an engine failure! Bertie true. Can't think of one off the top of my head, though! Bertie Any A/C that the gear rotates 90 degrees to stow would have greater drag during the "Rotate/Stow" sequence. Ralph Nesbitt Well, I ws thinking more of ther gear doors opeing and closing during the sequence. Bertie which in Tarverworld would mean that the transitioning gear doors, creating drag, would therefore be acting like a spolier and seeing that a spolier is a flap will make the wing thicker therfore creating lift. ergo a gear door is a lift device ! |
Greater lift for aircraft
(running with scissors) wrote
in om: Bertie the Bunyip wrote in message . .. "Ralph Nesbitt" wrote in : "Bertie the Bunyip" wrote in message ws.com... (running with scissors) wrote in om: Bertie the Bunyip wrote in message . .. (running with scissors) wrote in om: Bertie the Bunyip wrote in message . .. "mbrookesn231" wrote in le.rogers.c om: That makes no sense, according to that theory the wheel should lower the amount of lift, seeing as the lower part of the wheel is going in the direction of the air. nope, he's right, It's the greater speed of the upper part of the wheel that would increase it but it's insignificant in any case. Bertie the amount of theoretical lift generated is negligible, whereas the drag generated from extended gear is not Well, exactly. though on some aircraft the drag caused during retraction is considered worse than leaving it down in the event of an engine failure! Bertie true. Can't think of one off the top of my head, though! Bertie Any A/C that the gear rotates 90 degrees to stow would have greater drag during the "Rotate/Stow" sequence. Ralph Nesbitt Well, I ws thinking more of ther gear doors opeing and closing during the sequence. Bertie which in Tarverworld would mean that the transitioning gear doors, creating drag, would therefore be acting like a spolier and seeing that a spolier is a flap will make the wing thicker therfore creating lift. ergo a gear door is a lift device ! Snort! Bertie |
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