Today's Message Index:
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1. 06:44 AM - Re: Re: Searching for M-14P Exhaust System & Nanchang Header Tank (Kelley Monroe)
2. 02:48 PM - Re: Searching for M-14P Exhaust System & Nanchang Header Tank (Ttail)
3. 07:32 PM - Re: Re: Flying at the edge of the envelope, VGs whistle. (Warren Hill)
Message 1
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| Subject: | Re: Searching for M-14P Exhaust System & Nanchang Header |
Tank
I need an engine first.
Sent from my iPhone
> On Apr 6, 2019, at 8:48 PM, "greg.barnhard@gmail.com" <greg.barnhard@gmail.com>
wrote:
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> Did you find an exhaust? I have one off a Yak 52.
>
> Greg
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> Read this topic online here:
>
> http://forums.matronics.com/viewtopic.php?p=488589#488589
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Message 2
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| Subject: | Re: Searching for M-14P Exhaust System & Nanchang Header Tank |
Try Kimbals for the exhaust
https://www.jimkimballenterprises.com/index.php
I purchased a Stainless Steel Exhaust set for the CJ6/M14 combination around 3
years ago.
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=488601#488601
Message 3
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| Subject: | Re: Flying at the edge of the envelope, VGs whistle. |
Here are the images of the VGs on the vertical stabilizer and the
underside of the horizontal stabilizer. Their spacing for these is less
critical and Charles White provides a template for placement. When you
get these, suggest having a handful of spares just in case one comes
off.
Hope this helps,
Warren Hill
N464TW
Mesa, AZ
> On Mar 31, 2019, at 4:51 PM, Warren Hill <hill@doctor-hill.com
<mailto:hill@doctor-hill.com>> wrote:
>
> Will take some pictures the next time I=99m at the airport. The
placement of the VGs on the vertical stabilizer and the horizontal
stabilizer is not critical and the company supplies a generic template
for this. Here is their contact information.
>
> https://microaero.com <https://microaero.com/>
>
> Some meaningful insights into how all of this influences the
performance of the wing came during testing with yarn tufting. This
allows for visualization of the boundary layer breaking down as the
stall is approached. Attached is an image taken form the rear cockpit as
the stall was developing around 57 KIAS. By 55 KIAS, the airflow pattern
was completely disrupted out halfway between the dihedral break and
inboard edge of the aileron.
>
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> <DSC03587.JPG>
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>
>> On Mar 31, 2019, at 10:19 AM, motoadve <motoadve@racsa.co.cr
<mailto:motoadve@racsa.co.cr>> wrote:
>>
<mailto:motoadve@racsa.co.cr>>
>>
>> Can you show me pictures of were are they installed in the vertical
fin and horizontal stab?
>> Mine only has them on the wing, wonder if under the horizontal stab
will increase the reduction in stall speed even more.
>>
>> --------
>> www.Backcountry182.com <http://www.backcountry182.com/>
>> Cessna 182 P
>> CJ -6
>>
>>
>>
>>
>> Read this topic online here:
>>
>> http://forums.matronics.com/viewtopic.php?p=488379#488379
<http://forums.matronics.com/viewtopic.php?p=488379#488379>
>>
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