REFLECTOR: Plume Drag
Jeff Barnes via Reflector
reflector at tvbf.org
Fri Jul 4 21:23:02 CDT 2014
Hi Geoff,
If your pipes were just sticking out perpendicular to the plane, you have nearly one of worst drag configurations: CYLINDERS. A cylinder is .95 the drag of a flat plate, in other words, damn near as bad.
Look at Jean Prudhommes exhaust in the upload section of TVBF.ORG,
Regards,
Jeff Barnes
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From: Brian Michalk via Reflector <reflector at tvbf.org>
To: Velocity Aircraft Owners and Builders list <reflector at tvbf.org>
Sent: Friday, July 4, 2014 8:41 PM
Subject: Re: REFLECTOR: Plume Drag
How far away from the prop was your exhaust exit?
On 07/04/2014 05:15 PM, Geoff Gerhardt via Reflector wrote:
I changed my exhaust from the typical perpendicular to the fuselage to exiting out the back inside the cowl and did see a significant improvement (6-8ktas). I think its a combination of plume drag as well as disturbing the air going into the prop.
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>I am currently re-jiggering my exhaust again, this time exiting out the bottom of the cowling rather than inside the cowling (similar to what Brett described). I have the factory exhaust fairings (VEFL-01 and VEFR-01) and I'm just in the process of modifying my cowl to add them. I found the scorching of the prop excessive with it venting in the cowl. With a three bladed prop and the exhaust pipes located 180deg apart, there's no way to clock the prop so one blade doesn't get a hot exhaust blast. By moving the exhaust to exit below the cowl I'm hoping that I get less prop scorching. I don't mind cleaning off the soot, but I was getting enough heat effect on my Catto prop so that I could see it was affecting the fiberglass.
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>Geoff
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>On Thu, Jul 3, 2014 at 12:02 PM, Brian Michalk via Reflector <reflector at tvbf.org> wrote:
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>I just finished an email conversation with Marc Zeitlin on plume drag.
>>
>>My question to him was if he knew of any references to
research in this area. He does not, but believes the reason
for why people think plume drag exists is due to three
factors.
>>
>>1) Perpendicular pipes at the fuselage will have some
portion impacting free air, and will therefore have some
parasitic drag. If the tubes are arranged such that they do
not impinge free air, then there is no associated parasitic
drag. This would be the directly aft configuration where
tubes never really leave the cowl envelope.
>>2) There is some thrust to be gained from pointing the
exhaust aft. I'm not claiming its much, but I acknowledge
this. Not pointing it aft is wasting that extra little bit
of thrust.
>>3) Perpendicular ejection of exhaust will cause some
separated flow from the fuselage due to the exhaust plume,
increasing parasitic drag.
>>
>>He agrees that the plume itself cannot cause the drag,
because it's not attached to the airplane, but there could
be other factors increasing drag, and two of them have
nothing at all to do with the plume.
>>
>>He also pointed me to this conversation:
>>http://copilotco.com/mail-archives/matronics.2003/msg53894.html
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