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On Sat, 15 Mar 2008 19:39:13 -0400, Dudley Henriques
wrote: I believe you are repeating wht I have said. I said that "dragging it in" generally refers to flying the approach in the area of reverse command or if you will behind the power curve. This is absolutely correct. Coffin corner is the area behind the curve where sink rate can't be stopped with power but requires reduction in angle of attack. For a perfect example of an aircraft in coffin corner, see the Edwards AFB accident involving a young AF pilot who got his F100 so deep into coffin corner behind the curve he couldn't recover the airplane; not enough air under him to reduce the angle of attack. He applied full burner but couldn't fly it out on power alone. Reduction of angle of attack was what he needed and he didn't have the room. THIS is the definition of coffin corner and it most certainly IS in the area of reverse command. I thought coffin corner was the point where if you go slower you stall and if you go faster you hit critical mach number? |
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Peter Clark wrote in
: On Sat, 15 Mar 2008 19:39:13 -0400, Dudley Henriques wrote: I believe you are repeating wht I have said. I said that "dragging it in" generally refers to flying the approach in the area of reverse command or if you will behind the power curve. This is absolutely correct. Coffin corner is the area behind the curve where sink rate can't be stopped with power but requires reduction in angle of attack. For a perfect example of an aircraft in coffin corner, see the Edwards AFB accident involving a young AF pilot who got his F100 so deep into coffin corner behind the curve he couldn't recover the airplane; not enough air under him to reduce the angle of attack. He applied full burner but couldn't fly it out on power alone. Reduction of angle of attack was what he needed and he didn't have the room. THIS is the definition of coffin corner and it most certainly IS in the area of reverse command. I thought coffin corner was the point where if you go slower you stall and if you go faster you hit critical mach number? Kind of , but the bottom side isn;t exactly a stall, it's also a mach buffet. the main distinction being it happens at a higher than normally indicated airspeed, and more crucially, a lesser angle of attack. The net effect is the same, but it's important to distinguish between the two since the picture when it happens is substantially different. Just in case any of you guys are thinking of a VLJ. Bertie |
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On Sun, 16 Mar 2008 09:25:24 -0400, Peter Clark
wrote: On Sat, 15 Mar 2008 19:39:13 -0400, Dudley Henriques wrote: I believe you are repeating wht I have said. I said that "dragging it in" generally refers to flying the approach in the area of reverse However: ormal and short field landin gin the Bo...F33, Deb, and A36 (IF flown according to the POH) are all at well less than maximum endurance. This is far from dragging it in which was giving the ASF fits about "dragging it in for short field landings" which are flown well under max endurance speed, but are "steep". The short field is just steeper with more power. However in neither case should the plane be in the so called coffin corner as there is enough reserve power to stop the descent without lowering the nose. That is even flying a very steep short field approach. command or if you will behind the power curve. This is absolutely correct. Coffin corner is the area behind the curve where sink rate can't be stopped with power but requires reduction in angle of attack. Any of the Bo's get really squirley when flown this way and for a competent pilot will provide suficient warning, but I'd sure not want to get one that slow any where on final as that sucker is so close to stalling the unwary could quickly ruin their insurance companie's day. For a perfect example of an aircraft in coffin corner, see the Edwards AFB accident involving a young AF pilot who got his F100 so deep into coffin corner behind the curve he couldn't recover the airplane; not That was one impressive film strip. Although it w asn't long it sure seemed that way. He did one whale of a job balancing on the tail until she finally fell over to the left as I recall. When I say balancing on the tail, for those who haven't seen the video/film clip he wasn't just nose high. enough air under him to reduce the angle of attack. He applied full burner but couldn't fly it out on power alone. Reduction of angle of attack was what he needed and he didn't have the room. THIS is the definition of coffin corner and it most certainly IS in the area of reverse command. Which reminds me, I saw a clip of a 104 where I believe the engine seized. It started to skid sideways and then *flipped" over onto its top. Do you know the story behind that? I thought coffin corner was the point where if you go slower you stall and if you go faster you hit critical mach number? Roger Halstead (K8RI & ARRL life member) (N833R, S# CD-2 Worlds oldest Debonair) www.rogerhalstead.com |
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On Sun, 16 Mar 2008 09:25:24 -0400, Peter Clark
wrote: On Sat, 15 Mar 2008 19:39:13 -0400, Dudley Henriques wrote: I believe you are repeating wht I have said. I said that "dragging it in" generally refers to flying the approach in the area of reverse command or if you will behind the power curve. This is absolutely Well, time to try again. I had this ready to go and the computer ate it. When flying a Debonair, F-33, and A36 Bo by the POH all landings are done well below the max endurance speed, but not to the point where they don't have enough reserve power to arrest or even change the descent into a climb. They are however in the area where power controls rate of descent and pitch controls speed. correct. Coffin corner is the area behind the curve where sink rate can't be stopped with power but requires reduction in angle of attack. For a perfect example of an aircraft in coffin corner, see the Edwards AFB accident involving a young AF pilot who got his F100 so deep into coffin corner behind the curve he couldn't recover the airplane; not I saw the video and he did one whale of a job balancing on the thrust/tail until he lost it. He just needed a few thousand pounds more thrust. enough air under him to reduce the angle of attack. He applied full burner but couldn't fly it out on power alone. Reduction of angle of attack was what he needed and he didn't have the room. THIS is the definition of coffin corner and it most certainly IS in the area of reverse command. I saw a clip of a 104 that was skidding sideways and then flipped over on its top. I believe the engine seized on that one. any thought? I thought coffin corner was the point where if you go slower you stall and if you go faster you hit critical mach number? Roger Halstead (K8RI & ARRL life member) (N833R, S# CD-2 Worlds oldest Debonair) www.rogerhalstead.com |
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Roger wrote:
On Sun, 16 Mar 2008 09:25:24 -0400, Peter Clark wrote: On Sat, 15 Mar 2008 19:39:13 -0400, Dudley Henriques wrote: I believe you are repeating wht I have said. I said that "dragging it in" generally refers to flying the approach in the area of reverse command or if you will behind the power curve. This is absolutely Well, time to try again. I had this ready to go and the computer ate it. When flying a Debonair, F-33, and A36 Bo by the POH all landings are done well below the max endurance speed, but not to the point where they don't have enough reserve power to arrest or even change the descent into a climb. They are however in the area where power controls rate of descent and pitch controls speed. correct. Coffin corner is the area behind the curve where sink rate can't be stopped with power but requires reduction in angle of attack. For a perfect example of an aircraft in coffin corner, see the Edwards AFB accident involving a young AF pilot who got his F100 so deep into coffin corner behind the curve he couldn't recover the airplane; not I saw the video and he did one whale of a job balancing on the thrust/tail until he lost it. He just needed a few thousand pounds more thrust. enough air under him to reduce the angle of attack. He applied full burner but couldn't fly it out on power alone. Reduction of angle of attack was what he needed and he didn't have the room. THIS is the definition of coffin corner and it most certainly IS in the area of reverse command. I saw a clip of a 104 that was skidding sideways and then flipped over on its top. I believe the engine seized on that one. any thought? I thought coffin corner was the point where if you go slower you stall and if you go faster you hit critical mach number? Roger Halstead (K8RI & ARRL life member) (N833R, S# CD-2 Worlds oldest Debonair) www.rogerhalstead.com I think it's in the pilot's code that we're not allowed to say the airplane flipped over on it's "top" :-)))) -- Dudley Henriques |
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On Mar 16, 7:31 pm, Roger wrote:
.... I saw the video and he did one whale of a job balancing on the thrust/tail until he lost it. He just needed a few thousand pounds more thrust. I think some tape of that incident was used in this movie, http://www.imdb.com/title/tt0048364/ enough air under him to reduce the angle of attack. He applied full burner but couldn't fly it out on power alone. Reduction of angle of attack was what he needed and he didn't have the room. THIS is the definition of coffin corner and it most certainly IS in the area of reverse command. I saw a clip of a 104 that was skidding sideways and then flipped over on its top. I believe the engine seized on that one. any thought? I have a clip from "Planes of Flame", where the 104 is tangled in an arrestor net, yaws left, then rolls over right that looked messy. Is that the clip you mean? Ken Roger Halstead (K8RI & ARRL life member) (N833R, S# CD-2 Worlds oldest Debonair)www.rogerhalstead.com |
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Bertie the Bunyip wrote:
"Ken S. Tucker" wrote in news:e7b02c3d-eb33-4b04- : On Mar 16, 7:31 pm, Roger wrote: ... I saw the video and he did one whale of a job balancing on the thrust/tail until he lost it. He just needed a few thousand pounds more thrust. I think some tape of that incident was used in this movie, http://www.imdb.com/title/tt0048364/ enough air under him to reduce the angle of attack. He applied full burner but couldn't fly it out on power alone. Reduction of angle of attack was what he needed and he didn't have the room. THIS is the definition of coffin corner and it most certainly IS in the area of reverse command. I saw a clip of a 104 that was skidding sideways and then flipped over on its top. I believe the engine seized on that one. any thought? I have a clip from "Planes of Flame", where the 104 is tangled in an arrestor net, yaws left, then rolls over right that looked messy. Is that the clip you mean? Ken Roger Halstead (K8RI & ARRL life member) (N833R, S# CD-2 Worlds oldest Debonair)www.rogerhalstead.com A whole post where you didn't say anything idiotic. this must be a first, kennie! Bertie There does seem to be some improvement here. :-) -- Dudley Henriques |
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On Mar 16, 8:45 pm, Dudley Henriques wrote:
Bertie the Bunyip wrote: "Ken S. Tucker" wrote in news:e7b02c3d-eb33-4b04- : On Mar 16, 7:31 pm, Roger wrote: ... I saw the video and he did one whale of a job balancing on the thrust/tail until he lost it. He just needed a few thousand pounds more thrust. I think some tape of that incident was used in this movie, http://www.imdb.com/title/tt0048364/ enough air under him to reduce the angle of attack. He applied full burner but couldn't fly it out on power alone. Reduction of angle of attack was what he needed and he didn't have the room. THIS is the definition of coffin corner and it most certainly IS in the area of reverse command. I saw a clip of a 104 that was skidding sideways and then flipped over on its top. I believe the engine seized on that one. any thought? I have a clip from "Planes of Flame", where the 104 is tangled in an arrestor net, yaws left, then rolls over right that looked messy. Is that the clip you mean? Ken Roger Halstead (K8RI & ARRL life member) (N833R, S# CD-2 Worlds oldest Debonair)www.rogerhalstead.com A whole post where you didn't say anything idiotic. this must be a first, kennie! Bertie ****-OFF QUEER There does seem to be some improvement here. :-) Dudley Henriques DITTO |
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"Ken S. Tucker" wrote in
: On Mar 16, 8:45 pm, Dudley Henriques wrote: Bertie the Bunyip wrote: "Ken S. Tucker" wrote in news:e7b02c3d-eb33-4b04- : On Mar 16, 7:31 pm, Roger wrote: ... I saw the video and he did one whale of a job balancing on the thrust/tail until he lost it. He just needed a few thousand pounds more thrust. I think some tape of that incident was used in this movie, http://www.imdb.com/title/tt0048364/ enough air under him to reduce the angle of attack. He applied full burner but couldn't fly it out on power alone. Reduction of angle of attack was what he needed and he didn't have the room. THIS is the definition of coffin corner and it most certainly IS in the area of reverse command. I saw a clip of a 104 that was skidding sideways and then flipped over on its top. I believe the engine seized on that one. any thought? I have a clip from "Planes of Flame", where the 104 is tangled in an arrestor net, yaws left, then rolls over right that looked messy. Is that the clip you mean? Ken Roger Halstead (K8RI & ARRL life member) (N833R, S# CD-2 Worlds oldest Debonair)www.rogerhalstead.com A whole post where you didn't say anything idiotic. this must be a first, kennie! Bertie ****-OFF QUEER That's more like it k00kie boi. There does seem to be some improvement here. :-) Dudley Henriques DITTO Ooow! I sense some insecurity here. Want to talk about it, Kennie? Go on, you know you want to. Bertie |
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