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#51
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kage wrote:
"Newps" wrote in message ... kage wrote: On any standard light aircraft wing, all best climbs (rate of climb Vy, and angle of climb Vx) are achieved with a clean wing. Adding flaps causes the climb angle and rate to decrease. Not on my 182. The manual says, and I quote... Using 20 degree wing flaps reduces the ground run and total distance over the obstacle by approx 20 percent. Yes over an obstacle. But that is a compromise. On a short strip the compromise is less climb for shorter takeoff distance. Your 182 manual NEVER says that Vx is with flaps. NOWHERE! Vx in a 182 is clean wing. Read the POH. kage, You've made that statement a couple of times as if it means something. I'm not saying it doesn't mean anything, but when you've been asked to clarify, you respond with more authoritarian statements that don't explain. It's as if you expect us to just accept your authority. It seems to me that somone can define a term, say Vx, and -define- it to be whatever he wants. OK, so then you can authoritatively say that that's what Vx means, but so what? The part I am missing is: supposing I accept your statement that "Vx is a clean wing". How am I supposed to reason from that starting point to the place where you seem to want me to go, that best angle of climb is achieved with a clean wing? Thanks, Dave |
#52
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kage wrote: "Newps" wrote in message ... kage wrote: On any standard light aircraft wing, all best climbs (rate of climb Vy, and angle of climb Vx) are achieved with a clean wing. Adding flaps causes the climb angle and rate to decrease. Not on my 182. The manual says, and I quote... Using 20 degree wing flaps reduces the ground run and total distance over the obstacle by approx 20 percent. Yes over an obstacle. Well that's what were talking about...what gets me the highest in the air in the shortest distance over the ground. My owners manual says I get to 50 feet in 20% less distance than no flaps. Can't be more clearer than that. But that is a compromise. No, it's not. I want to be the highest in the air as possible over the shortest total ground distance. That will be with flaps 20. |
#53
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"Dave Butler" wrote in message ... kage wrote: "Newps" wrote in message I don't see what is difficult to understand. Vx is defined as best angle of climb. Do you have a hard time understanding that concept? The Cessna's and Piper's discussed here have POH's. The older ones have owners manuals. In each of these documents Vx is listed. It is always listed as a clean wing speed. Do you have difficulty with "clean wing?" Thus, anytime you lower flaps, climb angle is reduced. I know you don't want to believe that, and you are just playing dumb. Are you too lazy to just look in your POH? Karl |
#54
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"Newps" wrote in message ... kage wrote: "Newps" wrote in message ... kage wrote: On any standard light aircraft wing, all best climbs (rate of climb Vy, and angle of climb Vx) are achieved with a clean wing. Adding flaps causes the climb angle and rate to decrease. Not on my 182. The manual says, and I quote... Using 20 degree wing flaps reduces the ground run and total distance over the obstacle by approx 20 percent. Yes over an obstacle. Well that's what were talking about...what gets me the highest in the air in the shortest distance over the ground. My owners manual says I get to 50 feet in 20% less distance than no flaps. Can't be more clearer than that. But that is a compromise. No, it's not. I want to be the highest in the air as possible over the shortest total ground distance. That will be with flaps 20. It is most certainly a compromise, since you never accelerate to Vx. Your speed is just a climb speed to clear close in obsticles, and is not related to Vx. Once clear of those close in obstacles you will want to accelerate to Vx and retract flaps if you want to continue to climb at best angle. Simple concept. |
#55
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On Fri, 19 Nov 2004 15:01:57 -0700, Newps wrote:
kage wrote: "Newps" wrote in message ... kage wrote: On any standard light aircraft wing, all best climbs (rate of climb Vy, and angle of climb Vx) are achieved with a clean wing. Adding flaps causes the climb angle and rate to decrease. Not on my 182. The manual says, and I quote... Using 20 degree wing flaps reduces the ground run and total distance over the obstacle by approx 20 percent. Yes over an obstacle. Well that's what were talking about...what gets me the highest in the air in the shortest distance over the ground. My owners manual says I get to 50 feet in 20% less distance than no flaps. Can't be more clearer than that. But that is a compromise. No, it's not. I want to be the highest in the air as possible over the shortest total ground distance. That will be with flaps 20. Just can't resist jumping in here. Your climb gradient with flaps will be lower than with zero flaps. The only reason that you do better over a 50 ft obstacle is that your ground run is shortened so much (in a 182) that it more than makes up for the shallower climb to 50 AGL. Most 172's, for example, are better without flaps, even over a (standard) 50 ft obstacle (per their POH's). |
#56
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#57
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Jay Somerset wrote:
Just can't resist jumping in here. Your climb gradient with flaps will be lower than with zero flaps. Best angle of climb is determined by what gives you the most excess thrust. Best rate of climb is determined b what gives you the most excess power. |
#58
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"Roy Page" wrote in message ink.net...
So the question is. How long is a "short field" for a PA28-181 ? And for that matter how does that relate to a PA28-140 with 30 less horses. At sea level or up to maybe ~ 1500MSL field elevations and at "reasonable" density altitudes, I'd say short field would in an Archer would be runways under 2500' long. A few years ago before I got my PPASEL, I used to ride often with a fellow who operated a Cherokee 140 out of a 2000' private grass strip in the middle of Texas. Even in the summer time, the 140 had no problems with the two of us on board with fuel to the tabs. We were nowhere near max gross however, and had no obstacles to clear at either end of the airstrip. |
#59
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Gentlemen,
I really appreciate all the informed and learned replies to my question. I know my Archer pretty well, and have flown rental Archers for a number of years. The POH is totally clear on the techniques regarding take-off and the use of flaps. I did not intend to ask questions which the POH properly covers. My question is much more simple. Where can I find the definition for a "Short Field" as referred to in my POH. The POH makes no attempt to define the length of the short field. That's all I need guys, Where can I find either a defined formulae or Piper specific definition of a "Short Field" Thanks for all the great input that this question has created. -- Roy N5804F - PA28-181 have pored a POH and "One's Too Many" wrote in message om... "Roy Page" wrote in message ink.net... So the question is. How long is a "short field" for a PA28-181 ? And for that matter how does that relate to a PA28-140 with 30 less horses. At sea level or up to maybe ~ 1500MSL field elevations and at "reasonable" density altitudes, I'd say short field would in an Archer would be runways under 2500' long. A few years ago before I got my PPASEL, I used to ride often with a fellow who operated a Cherokee 140 out of a 2000' private grass strip in the middle of Texas. Even in the summer time, the 140 had no problems with the two of us on board with fuel to the tabs. We were nowhere near max gross however, and had no obstacles to clear at either end of the airstrip. |
#60
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Roy Page wrote: Where can I find the definition for a "Short Field" as referred to in my POH. No such thing. The POH makes no attempt to define the length of the short field. Because it's a moving target. Weight, wind and air density all affect performance. |
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