Today's Message Index:
----------------------
 
     1. 01:41 PM - Re: Sky Scout Plans (taildrags)
     2. 02:12 PM - Re: Re: Sky Scout Plans (Steven Dortch)
     3. 02:53 PM - Re: Re: Sky Scout Plans ((null) raykrause)
     4. 06:49 PM - Re: Re: Sky Scout Plans (Richard Schreiber)
     5. 08:20 PM - Re: Sky Scout Plans (taildrags)
 
 
 
Message 1
| 					INDEX |  Back to Main INDEX |  
| 					NEXT |  Skip to NEXT Message |  
| 	LIST |  Reply to LIST Regarding this Message |  
| 		SENDER |  Reply to SENDER Regarding this Message |  
  | 
      
      
| Subject:  | Re: Sky Scout Plans | 
      
      
      Just measured the deck angle of my airplane with it sitting on the ground in 3-point
      attitude: almost exactly 11 degrees.  Knowing now that my wing is set with
      about 1 degree less incidence than it should have, I think I need to get the
      nose a bit higher.  I had already been thinking about getting some slightly
      fatter tires (does anybody happen to know what size tires are on NX13691, "The
      Allen Rudolph Piet"?)- mine are 6.00x6 and I'm looking at some 8.00x6 weenies.
      
      Somewhere or the other I have a comparative analysis of the Piet airfoil vs. the
      Cub's USA35B and I'm curious as to what the lift looks like vs. the Piet at
      the same angle of attack.   Jack wrote that the Cub has a 13 degree deck angle
      and that puts the wing close to the critical AOA, so I should be able to get
      some good info out of that comparison.
      
      --------
      Oscar Zuniga
      Medford, OR
      Air Camper NX41CC "Scout"
      A75 power, 72x36 Culver prop
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=473170#473170
      
      
Message 2
| 					INDEX |  Back to Main INDEX |  
| 				PREVIOUS |  Skip to PREVIOUS Message |  
| 					NEXT |  Skip to NEXT Message |  
| 	LIST |  Reply to LIST Regarding this Message |  
| 		SENDER |  Reply to SENDER Regarding this Message |  
  | 
      
      
| Subject:  | Re: Sky Scout Plans | 
      
      Oscar, to get 15 degree deck angle, I had to jack my Pietenpol up quite a
      bit. I will check the angle when I go out next.
      
      Blue Skies,
      
      
      On Wed, Sep 27, 2017 at 3:41 PM, taildrags <taildrags@hotmail.com> wrote:
      
      >
      > Just measured the deck angle of my airplane with it sitting on the ground
      > in 3-point attitude: almost exactly 11 degrees.  Knowing now that my wing
      > is set with about 1 degree less incidence than it should have, I think I
      > need to get the nose a bit higher.  I had already been thinking about
      > getting some slightly fatter tires (does anybody happen to know what size
      > tires are on NX13691, "The Allen Rudolph Piet"?)- mine are 6.00x6 and I'm
      > looking at some 8.00x6 weenies.
      >
      > Somewhere or the other I have a comparative analysis of the Piet airfoil
      > vs. the Cub's USA35B and I'm curious as to what the lift looks like vs. the
      > Piet at the same angle of attack.   Jack wrote that the Cub has a 13 degree
      > deck angle and that puts the wing close to the critical AOA, so I should be
      > able to get some good info out of that comparison.
      >
      > --------
      > Oscar Zuniga
      > Medford, OR
      > Air Camper NX41CC "Scout"
      > A75 power, 72x36 Culver prop
      >
      >
      > Read this topic online here:
      >
      > http://forums.matronics.com/viewtopic.php?p=473170#473170
      >
      >
      
      
      -- 
      Blue Skies,
      Steve D
      
Message 3
| 					INDEX |  Back to Main INDEX |  
| 				PREVIOUS |  Skip to PREVIOUS Message |  
| 					NEXT |  Skip to NEXT Message |  
| 	LIST |  Reply to LIST Regarding this Message |  
| 		SENDER |  Reply to SENDER Regarding this Message |  
  | 
      
      
| Subject:  | Re: Sky Scout Plans | 
      
      Oscar,
      
      So at what deck angle do most Piets stall? Did I miss something?  My SkyScou
      t's 3-point deck angle is 14-14.5 degrees.  Seems pretty steep. My 7AC is ab
      out 12 degrees and I don't know where it stalls power-off. But it seems quit
      e a bit higher that the 3-point angle.
      
      I will have to deflate my tires a bit....since the brakes might be pretty lo
      usy!  I will test taxi as soon as I patch a hole in the wing. Damn antenna o
      n the Waiex!
      
      Does anyone remember the pounds of pull on the "Official Fish Scale" that ha
      s been ruled to be adequate? I don't have the "Official" scale. But one simi
      lar!  Could not be too far off!
      
      Ray Krause
      
      Sent from my iPad
      
      > On Sep 27, 2017, at 2:10 PM, Steven Dortch <steven.d.dortch@gmail.com> wro
      te:
      > 
      > Oscar, to get 15 degree deck angle, I had to jack my Pietenpol up quite a b
      it. I will check the angle when I go out next. 
      > 
      > Blue Skies,
      > 
      > 
      >> On Wed, Sep 27, 2017 at 3:41 PM, taildrags <taildrags@hotmail.com> wrote:
      
      
      >> 
      >> Just measured the deck angle of my airplane with it sitting on the ground
       in 3-point attitude: almost exactly 11 degrees.  Knowing now that my wing i
      s set with about 1 degree less incidence than it should have, I think I need
       to get the nose a bit higher.  I had already been thinking about getting so
      me slightly fatter tires (does anybody happen to know what size tires are on
       NX13691, "The Allen Rudolph Piet"?)- mine are 6.00x6 and I'm looking at som
      e 8.00x6 weenies.
      >> 
      >> Somewhere or the other I have a comparative analysis of the Piet airfoil v
      s. the Cub's USA35B and I'm curious as to what the lift looks like vs. the P
      iet at the same angle of attack.   Jack wrote that the Cub has a 13 degree d
      eck angle and that puts the wing close to the critical AOA, so I should be a
      ble to get some good info out of that comparison.
      >> 
      >> --------
      >> Oscar Zuniga
      >> Medford, OR
      >> Air Camper NX41CC "Scout"
      >> A75 power, 72x36 Culver prop
      >> 
      >> 
      >> 
      >> 
      >> Read this topic online here:
      >> 
      >> http://forums.matronics.com/viewtopic.php?p=473170#473170
      >> 
      >> 
      >> 
      >> 
      >> 
      >> 
      >> =========================
      >> br> enpol-List" rel="noreferrer" target="_blank">http://www.matronics
      .com/Navigator?Pietenpol-List
      >> =========================
      >> FORUMS -
      >> eferrer" target="_blank">http://forums.matronics.com
      >> =========================
      >> WIKI -
      >> errer" target="_blank">http://wiki.matronics.com
      >> =========================
      >> b Site -
      >>           -Matt Dralle, List Admin.
      >> rel="noreferrer" target="_blank">http://www.matronics.com/contributio
      n
      >> =========================
      >> 
      >> 
      >> 
      > 
      > 
      > 
      > -- 
      > Blue Skies,
      > Steve D
      
Message 4
| 					INDEX |  Back to Main INDEX |  
| 				PREVIOUS |  Skip to PREVIOUS Message |  
| 					NEXT |  Skip to NEXT Message |  
| 	LIST |  Reply to LIST Regarding this Message |  
| 		SENDER |  Reply to SENDER Regarding this Message |  
  | 
      
      
| Subject:  | Re: Sky Scout Plans | 
      
      
      Oscar,
      
      There was some discussion at Brodhead this year about this very thing. 
      The few builders I talked to all agreed that the critical AOA on a Piet 
      should be around 12.5 degrees for the deck angle. That being said , many 
      Piets are much less than that. On mine, my deck angle is 12.5 degrees. 
      With all the stuff I have under the tail post ---"A" frame, spring and 
      tail wheel, I had to make my gear legs a little longer to go that high. 
      NX478RS flys well, but there is no way I can step into the rear pit 
      without an attached step.
      
      Rick Schreiber
      NX478RS
      Valparaiso, IN
      
      On 9/27/2017 3:41 PM, taildrags wrote:
      >
      > Just measured the deck angle of my airplane with it sitting on the ground in
      3-point attitude: almost exactly 11 degrees.  Knowing now that my wing is set
      with about 1 degree less incidence than it should have, I think I need to get
      the nose a bit higher.  I had already been thinking about getting some slightly
      fatter tires (does anybody happen to know what size tires are on NX13691, "The
      Allen Rudolph Piet"?)- mine are 6.00x6 and I'm looking at some 8.00x6 weenies.
      >
      > Somewhere or the other I have a comparative analysis of the Piet airfoil vs.
      the Cub's USA35B and I'm curious as to what the lift looks like vs. the Piet at
      the same angle of attack.   Jack wrote that the Cub has a 13 degree deck angle
      and that puts the wing close to the critical AOA, so I should be able to get
      some good info out of that comparison.
      >
      > --------
      > Oscar Zuniga
      > Medford, OR
      > Air Camper NX41CC "Scout"
      > A75 power, 72x36 Culver prop
      >
      >
      > Read this topic online here:
      >
      > http://forums.matronics.com/viewtopic.php?p=473170#473170
      >
      >
      
      
Message 5
| 					INDEX |  Back to Main INDEX |  
| 				PREVIOUS |  Skip to PREVIOUS Message |  
| 					NEXT |  Skip to NEXT Message |  
| 	LIST |  Reply to LIST Regarding this Message |  
| 		SENDER |  Reply to SENDER Regarding this Message |  
  | 
      
      
| Subject:  | Re: Sky Scout Plans | 
      
      
      Steve D.- never said I wanted to get 15 degrees.  Others have said that anything
      over 13 is probably excessive.  That sounds like it's been echoed by several
      others, including Rick's comment about a general agreement from others about
      12.5 degrees being the target.
      
      Rick S.- my airplane has a step for getting into the rear cockpit... never tried
      "giant stride" stepping into it!  And since my deck angle is at 11 degrees,
      my airplane is about 1.5 degrees nose-down from optimum for full-stalling it in
      the 3-point attitude.  However, my wing is also set at 1 degree *less* incidence
      than the plans call for, so now my wing is about 2.5 degrees nose-down from
      optimum.  I'm going to try some larger tires (wanted to anyway), but just studying
      it in AutoCAD, I'll probably only get 1 to 1.5 degrees more deck angle,
      so I'll still be short of optimum but should be better.  This is experimental
      aviation!
      
      --------
      Oscar Zuniga
      Medford, OR
      Air Camper NX41CC "Scout"
      A75 power, 72x36 Culver prop
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=473176#473176
      
      
 
Other Matronics Email List Services
 
 
These Email List Services are sponsored solely by Matronics and through the generous Contributions of its members.
 
 
-- Please support this service by making your Contribution today! --
  
 |