X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Mon, 20 Sep 2010 08:40:44 -0400 Message-ID: X-Original-Return-Path: Received: from smtpoutwbe11.prod.mesa1.secureserver.net ([208.109.78.27] verified) by logan.com (CommuniGate Pro SMTP 5.3.9) with SMTP id 4471801 for lml@lancaironline.net; Sat, 18 Sep 2010 12:01:02 -0400 Received-SPF: none receiver=logan.com; client-ip=208.109.78.27; envelope-from=wolfgang@micom.net Received: (qmail 8204 invoked from network); 18 Sep 2010 16:00:26 -0000 Received: from unknown (HELO localhost) (72.167.218.140) by smtpoutwbe11.prod.mesa1.secureserver.net with SMTP; 18 Sep 2010 16:00:26 -0000 Received: (qmail 7419 invoked by uid 99); 18 Sep 2010 16:00:26 -0000 Content-Transfer-Encoding: quoted-printable Content-Type: text/html; charset="utf-8" X-Originating-IP: 65.198.5.99 User-Agent: Web-Based Email 5.2.31 X-Original-Message-Id: <20100918090026.32641d4b5e18c0a8912b240205ca344f.99db09bc6b.wbe@email04.secureserver.net> From: X-Original-To: lml@lancaironline.net Subject: RE: [LML] Re: In need more H.P. X-Original-Date: Sat, 18 Sep 2010 09:00:26 -0700 Mime-Version: 1.0
More horsepower is the expensive and limited way of going faster.=
Reducing drag is the "free" way of going faster.
 
I have recently collected some more test information about the drag bu= cket on the 320.
With the information so far, it looks like 160K is the high end of the= drag bucket with the flaps at 7 deg. reflex.
I have not yet tried to re-rig for 10 deg reflex which should yield so= me more "free" speed at the high end. More reflex basically lowers the desi= gn coeficient of lift.
 
Another way to get some more speed is to reduce the wing area like Rea= r Bear but that approach is a bit more involved and will have consequences = by requiring higher landing speeds. :-(
 
Wolfgang
 
------ Original Message --------
Subject: Re: [LML] Re: In need mor= e H.P.
From: CavittP@aol.com
D= ate: Fri, September 17, 2010 6:39 am
To: lml@lancaironline.net

Thanks everyone for the input. I really appreciate your taking th= e time to answer my post.  Some solid ideas for me to consider.&n= bsp;
 
Probably will first try to resurrect my LSE Plasma III ignition system= but this time use the case mounted flywheel sensor instead of the original= pad mounted one that seemed to be sensitive to the heat buildup in the are= a of the accessories.  Will also try to relocate the computer to a mor= e forward location to keep all the leads lengths to a minimum.  I've a= lways run Bendix mags.
 
Already use gap seals but may change cowling openings from the 235 con= figuration to the 320 style.  My CHT's run quite cool, so am cert= ain there is too much cooling drag.   I'm consistently = getting 180-185 KTAS (dependent on temperature) at 2700 RPM (full throttle)= at 7,500' & 8,500' MSL with my 150 HP O-320-E2D and Aymar-Demuth 62 X = 78 propeller. 
 
With power settings for 170 KTAS, I have a range of near 1000 NM&= nbsp;(6.5 hours) with the 54 gallons of usable fuel at 8,500'-9,500' MSL (7= hours to dry tanks).  Have on several occasions flown non-stop from S= an Diego to Seattle and on the way back as well (that leg was usually 5.5 -= 6 hours).
 
When the time comes for an overhaul will consider replacing the engine= with an O-360 or 390 and will switch to a CS prop at that time.  This= is probably what I really need to do, but my engine is still running great= with very little oil consumption.
 
Thanks again!
 
Pete Cavitt - N320PL
619-701-0784 Cell
www.petecavitt.com
<= /DIV>