KIS-List Digest Archive

Fri 11/30/12


Total Messages Posted: 4



Today's Message Index:
----------------------
 
     0. 09:05 AM - [Please Read] - Last Official Day of List Fund Raiser! (Matt Dralle)
     1. 03:04 PM - Fw: Vortex gens. to Tim Yoder (Bob and Kathy)
     2. 08:49 PM - Pics of VG's on airplane (Flyinisfun@aol.com)
     3. 09:12 PM - Re: Pics of VG's on airplane (F. Tim Yoder)
 
 
 


Message 0


  • PREVIOUS
  • Skip to PREVIOUS Message
  • NEXT
  • Skip to NEXT Message
  • LIST
  • Reply to LIST Regarding this Message
  • SENDER
  • Reply to SENDER Regarding this Message
    Time: 09:05:16 AM PST US
    From: Matt Dralle <dralle@matronics.com>
    Subject: [Please Read] - Last Official Day of List Fund Raiser!
    Dear Listers, Its November 30th and that always means a couple of things. Its my birthday again; number 49 actually! But it also means that its that last official day of the Matronics Email List Fund Raiser! If you been thinking about picking up one of those really nice incentive gifts now is the time to jump on it!! If you've been meaning to make a Contribution this month but have been putting it off for some reason, NOW is the time! I will be posting the List of Contributors in a few days, so you'll probably want to be known as a person that supported the Lists! I want to thank everyone that has so generously made a Contribution this year in support of our Lists. It is your generosity that keeps this operation running and I don't ever forget it. The List Contribution Web Site is fast and easy. Please support our habit by making your Contribution right now: http://www.matronics.com/contribution Or, by dropping a personal check in the mail to: Matt Dralle / Matronics 581 Jeannie Way Livermore CA 94550 Thank you to all in advance! Matt Dralle Matronics Email List Administrator


    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
    Time: 03:04:29 PM PST US
    From: Bob and Kathy <katebob10@yahoo.com>
    Subject: Fw: Vortex gens. to Tim Yoder
    =0A=0A=0A----- Forwarded Message -----=0AFrom: Bob and Kathy <katebob10@yah oo.com>=0ATo: "flyoder@yoderbuilt.com" <flyoder@yoderbuilt.com> =0ASent: Fr iday, November 30, 2012 10:05 AM=0ASubject: Vortex gens.=0A =0A=0AHi Tim. T he Vortex gen kit is by Harrison designs. They have a web page "landshorter .com"=0ATheir price is- $95.00 for the kit. Includes 100 pieces and instr uctions for experimental aircraft. This kit is complete and never used. The kit does not include adhesive but recommended type is included in instruct ions. I will take=0A$ 60.00 plus shipping. Bob


    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
    Time: 08:49:24 PM PST US
    From: Flyinisfun@aol.com
    Subject: Pics of VG's on airplane
    Here are pictures of the VG's on the wing and under the horizontal stabilizer. 1. The VG's are located on the underside of the horizontal stab. 4" ahead of the elevator hinge line, spaced 2.5" apart. They go the full width on each side. See photos. 2. The wing VG's are located on the top side, 10" back from a vertical line on the leading edge, starting about 20" outboard of the fuselage. This gives me space to get in and out of the cabin. I think I will add 2 or 3 near the fuselage for the fillet area. These are also spaced 2.5" apart. See photos. These are not scientifically placed but located in accordance to some information I found on the Internet which goes like this. With the plane in a level position, lay a straight edge level, front to rear, across the wing and where it breaks from the surface on the rear, measure 4" ahead of this point and put the leading edge of the VG's there. This is the method I used. Where the trailing edge of the straight edge seperates from the surface is the leading edge where the air begins to burble. The vortex needs to be started before this point and someone has come up with the 4" ahead of this point. This might not be true on all airfoils but I know it works here. Another way is to tuft the wing and find where the burble point begins. I think the 4" is an obituary point so who knows. Do I have the most optimum point, I really don't know but it works. If someone thinks they finds a better way to do this let me know. Jesse


    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
    Time: 09:12:59 PM PST US
    From: "F. Tim Yoder" <ftyoder@yoderbuilt.com>
    Subject: Re: Pics of VG's on airplane
    Jesse, Thanks, did you say what brand you used? Tim ----- Original Message ----- From: Flyinisfun@aol.com To: Kis-list@matronics.com Sent: Friday, November 30, 2012 9:48 PM Subject: KIS-List: Pics of VG's on airplane Here are pictures of the VG's on the wing and under the horizontal stabilizer. 1. The VG's are located on the underside of the horizontal stab. 4" ahead of the elevator hinge line, spaced 2.5" apart. They go the full width on each side. See photos. 2. The wing VG's are located on the top side, 10" back from a vertical line on the leading edge, starting about 20" outboard of the fuselage. This gives me space to get in and out of the cabin. I think I will add 2 or 3 near the fuselage for the fillet area. These are also spaced 2.5" apart. See photos. These are not scientifically placed but located in accordance to some information I found on the Internet which goes like this. With the plane in a level position, lay a straight edge level, front to rear, across the wing and where it breaks from the surface on the rear, measure 4" ahead of this point and put the leading edge of the VG's there. This is the method I used. Where the trailing edge of the straight edge seperates from the surface is the leading edge where the air begins to burble. The vortex needs to be started before this point and someone has come up with the 4" ahead of this point. This might not be true on all airfoils but I know it works here. Another way is to tuft the wing and find where the burble point begins. I think the 4" is an obituary point so who knows. Do I have the most optimum point, I really don't know but it works. If someone thinks they finds a better way to do this let me know. Jesse




    Other Matronics Email List Services

  • Post A New Message
  •   kis-list@matronics.com
  • UN/SUBSCRIBE
  •   http://www.matronics.com/subscription
  • List FAQ
  •   http://www.matronics.com/FAQ/KIS-List.htm
  • Web Forum Interface To Lists
  •   http://forums.matronics.com
  • Matronics List Wiki
  •   http://wiki.matronics.com
  • 7-Day List Browse
  •   http://www.matronics.com/browse/kis-list
  • Browse KIS-List Digests
  •   http://www.matronics.com/digest/kis-list
  • Browse Other Lists
  •   http://www.matronics.com/browse
  • Live Online Chat!
  •   http://www.matronics.com/chat
  • Archive Downloading
  •   http://www.matronics.com/archives
  • Photo Share
  •   http://www.matronics.com/photoshare
  • Other Email Lists
  •   http://www.matronics.com/emaillists
  • Contributions
  •   http://www.matronics.com/contribution

    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! --