X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from outbound-mail-341.bluehost.com ([66.147.249.2] verified) by logan.com (CommuniGate Pro SMTP 5.2.15) with SMTP id 3760880 for flyrotary@lancaironline.net; Wed, 15 Jul 2009 21:36:53 -0400 Received-SPF: pass receiver=logan.com; client-ip=66.147.249.2; envelope-from=jslade@canardaviation.com Received: (qmail 18677 invoked by uid 0); 16 Jul 2009 01:36:15 -0000 Received: from unknown (HELO host296.hostmonster.com) (66.147.240.96) by outboundproxy7.bluehost.com.bluehost.com with SMTP; 16 Jul 2009 01:36:15 -0000 DomainKey-Signature: a=rsa-sha1; q=dns; c=nofws; s=default; d=canardaviation.com; h=Received:Message-ID:Date:From:User-Agent:MIME-Version:To:Subject:References:In-Reply-To:Content-Type:Content-Transfer-Encoding:X-Identified-User; b=hml0PbXrireAc4LM9u9F8pFLE3APMS/+qPtR4CQLj5HQm/b86nsqe4zyGSoAdTWEVf+cPTWz8nOyMHoMbUHNVN4DGfB7PNFce+DSn7pZElEGSHkelIIDStrs9th7OPGh; Received: from c-76-108-115-200.hsd1.fl.comcast.net ([76.108.115.200] helo=[192.168.1.4]) by host296.hostmonster.com with esmtpsa (TLSv1:AES256-SHA:256) (Exim 4.69) (envelope-from ) id 1MRFtO-0001fT-Ta for flyrotary@lancaironline.net; Wed, 15 Jul 2009 19:36:15 -0600 Message-ID: <4A5E8402.8010007@canardaviation.com> Date: Wed, 15 Jul 2009 21:36:02 -0400 From: John Slade User-Agent: Thunderbird 1.5.0.14 (Windows/20071210) MIME-Version: 1.0 To: Rotary motors in aircraft Subject: Re: [FlyRotary] Re: Intake velocity, stack lengths. References: In-Reply-To: Content-Type: text/plain; charset=ISO-8859-1; format=flowed Content-Transfer-Encoding: 7bit X-Identified-User: {3339:host296.hostmonster.com:instanu1:canardaviation.com} {sentby:smtp auth 76.108.115.200 authed with jslade+canardaviation.com} Ben, If you're thinking of making a tube out of carbon fiber, this product may be of interest: http://www.fibreglast.com/showproducts-category-Carbon+Fiber+Fabric,+Tapes+&+Tow-15.html Scroll down to Braided Biaxial Sleeves. I used the Vinyl Ester product from this firm. Their customer support was excellent. Regards, John Slade George Lendich wrote: > Lynn, > I've often wondered how the air flow is affected by joined tubes, with > a slip tube outer. My concern is tripping the boundary layer and > causing turbulence enough to restrict flow. Is there any really good > way of achieving a nice consistent flow with such a join. > I thought of rounding off the inner facing edges, but then wondered > if that minor diameter increase would disturb the continuity of velocity. > Probably all a trade off. > George ( down under) > > Fellows, > > > > I have been thinking up this crazy idea of trying to make intake > > runner tubes out of carbon fiber. My question is regarding > length of > > the velocity stack. Does the length make a difference? Could a > > velocity stack be more or less the entire length of the tube? > > Meaning, if I have a 12" intake tube, could the entire length of > the > > tube be a gradual taper to the diameter of the block opening? > Would > > that mess with the speed the air is traveling in the tube? > > Aerodynamics is not something I have a very good handle on, and am > > hoping someone out there in Fly Rotary land can shed some light. > > > > Thoughts??? > > > > BTW, Any reasons why carbon fiber should not be used for intake > > tubes? May make the velocity tubes a mute point. > > > > Thanks for any thoughts. > > > > Ben Schneider > > > It would take the rest of your life to read all there is to read > about intake (tuned) lengths. So here is my view on it. > > The pipe organ idea is in play, but in my opinion is gifted too > much interest. In actual operation just about anything works prety > close to just fine. I just reviewed some formula Super Vee stuff > and note that a number of intakes were tried. Super Vee was a > class where a 1600 CC VW (Rabbit) engines were used in race cars. > The stock parts had to be used but could be modified by machining, > The intake runners could be up to 32MM, and the mechanical fuel > injection (probably from the diesel I think) could be used. > > HP well above 180 was the result, from VW parts. A straight 32MM > tube with a bellmouth. Not very exotic. > > The tuned length of any system has many harmonic peaks. They look > like the primary frequency but are removed from it by a factor of > 4. So you have harmonic peaks at multipals of 4. So, 4,8,16 and so > on. So there are secondarys that show up to either side of the > primary, and some of those are reenforced by combinations of the > secondaries, so the 16th harmonic can be quite clear and easy to > find on a scope. > > The outcome is that it would be foolish to build an intake with > one primary frequency in mind. Say you want to cruise at 6,000 > RPM, and built tubes to peak at that frequency. If you cannot keep > the engine at that RPM exactly, the effect is lost. Then you find > the engine in a null between peaks and performance is now less > than that of the thrown together mess on that plane in the next > hanger. > > On takoff you would want to have say 6,500 or 7,000 available. > Where would you tune for that? > > So I drop back to what works in most situations. In general long > columns of air operate at lower frequencies. Short columns at > higher frequencies. Large diameters at lower and small diameters > at higher, and so on. > > The ideal shape for intake runners is tapered. Yep, thats it. not > often seen due to complexity of construction, but if you want to > talk ideal................. > > The horn shape at the end of the tube is to prevent a vena > contracta that reduces the effective diameter of the tube. A short > rounded edge that turns back 180 degrees is the very best and > works well in confined spaces like a plenum. For carbs, not so > good. At harmonics of, and just off peak frequencies, you will get > a ball of fuel standing in space just outside of the horn. In > those cases, a longer tapered horn works better to cover up a > number of frequencies and make the ball less obvious. > > The tuned length thing works less well in bent systems, and since > the nearly best length will involve runners over the top of the > engine, there is at least a 180 turn involved, and for side port > engines, two turns involved. So, to start off we are in tuning > trouble with a bent system that tends to null our best math > picture of ideal. > > Round runners are ideal for efficiency in moving air through the > smallest cross section. However, in a turn > the "D" shape takes over from the round, in that the mass of the > airflow tends to move along the outer wall, and at some speeds may > be seen moving along the inside wall in the wrong direction, and > also may > slow and upset the flow along the outer wall. In most cases the > "D" shape may have slightly less cross section than the original > round runner. Also there may be improvements should a slightly > course or rough surface be left along the flat of the "D" so as to > keep flow attached and reduce the higher velocity along the > outside. Uniform velocity is better than a number of velocities or > even reversed flow. > > The taper............ > > Large tube diameters have lower velocity and small higher for any > fixed depression. If you imagine the rotor as a blade and the > intake flow as a sausage being pushed through the blade, then you > are one sick puppy............. > > However, it works for me. > > So would high velocity at the port face, (where the rotor cuts off > each chunk) be better than low velocity? > > The higher velocity for any unit of time means more sausage (or > fuel air mixture) entering the chamber. > > Yes high velocity is better. But drag in the runner develops at > the square of velocity, so if the runner is the same diameter for > all of its length, drag will be high, the boundary layer will be > thick and easy to upset. Suppose then that the taper was only in > the last several inches of the runner. Or if you want the ideal, > the taper starts at the horn and runs the length of the runner > tightening to the port size at the manifold face. Less drag > overal. Thinner more stable boundary layer, and the highest > possible velocity at the port face. > > Another thought.......... > > The primary and secondary ports feed just one rotor each set. The > primary ports are those in the center iron, and are smaller than > the secondary ports in the end irons. The engine operates for most > of its life on the primaries, as little HP is called for in normal > driving. The primaries are small, so as to maintain high velocity, > and crisp throttle response. > > I would join the two intake ports and run a single runner for each > rotor housing. Less volume consumed. > Lighter intake system. Smaller plenum. Probably no loss of > performance. The molded part then could be tapered, have the "D" > shape, the rough inside turn, a length of straight tube to mate to > a slip tube to "tune" runner lengths. > > Lynn E. Hanover > > > > >