Mailing List flyrotary@lancaironline.net Message #1727
From: Ed Anderson <eanderson@carolina.rr.com>
Sender: Marvin Kaye <marv@lancaironline.net>
Subject: Re: [FlyRotary] Tuned Induction
Date: Fri, 23 May 2003 17:42:52 -0400
To: <flyrotary>

----- Original Message -----
From: Al Gietzen
To: Rotary motors in aircraft
Sent: Thursday, May 22, 2003 5:10 PM
Subject: [FlyRotary] Tuned Induction



Al, I don't know much about induction systems and they appear to be as much "Magic" as science.

Obviously, I don’t either.  But I’d like to be able to get it out of the realm of magic.
 My own personal  story is that when I had a Weber throttle body with two 2" dia throats with a relative short length induction (about 1/2 my current length), my static rpm was 5000 rpm, my top speed was 182 MPH TAS and rate of climb was around 900 fpm.  When I created an intake using smaller (1 5/8 and 1 3/8" dia tubes) of the length that theoretically are tuned to provide the "dynamic charging effect" at 5900 rpm, my static went up to 5300 rpm, my ROC went up to 1200 fpm and my top speed to 196 MPH TAS.   So while I can't prove that my current induction system is better "tuned" to my operating regime and rpm - I sure like the improved results much better.

Given that speed goes by the cube root of HP; the speed change suggests that your power increased by 25%; so maybe something suspect there, or there was something really wrong with your original setup.  What else changed besides your runner length?


Al,
The changes were runner length (longer by approx 20%) and diameter of tubes (smaller by 25%).
 
After reading Paul Yaw's tech stuff about the importance of the velocity of the air/fuel mixture in an intake.  I calculated that on my original manifold (two 2" dia throats) that my intake velocity (assuming I was producing 180 HP which I defintely was NOT!) would have been approx 71 MPH.  According to what I read, you want much higer air velocity.  The theory (If I understood it) was that the interia of a faster moving slug of air/fule   would stuff more air/fuel mixture into the chamber than slower moving air/fuel mixture.  My change in tube diameter and length more than double my air velocity (calculated not measured) through the tubes and into the chamber

Below is an extract of Paul Yaws very understandable and excellent series on airflow for the rotary:

"....Velocity alone determines at what rpm peak torque and horsepower will occur for a given intake and exhaust duration. (Duration is the amount of time that the ports are open.) As most readers know, the intake port on a rotary engine closes well after bottom dead center.(BDC) What this means, is that the rotor is starting to compress the mixture while the port is still open. When velocity is low, some of the mixture will be squeezed back into the intake manifold. If velocity is high, the inertia of the incoming mixture will overcome the rising pressure of the chamber, and continue to pack mixture into the engine well after bdc. This effect is called inertial supercharging, and you can feel this while you are driving. At low speed, the engine does not make much torque, but as rpm increases, the engine really starts to put you back in your seat. The power increase that you are feeling is the result of the extra mixture being packed into the chamber as a result of higher intake velocity.

Now that you know how important velocity is, you must also understand that there is such a thing as excessive intake velocity. It has been determined that once the velocity in the induction system reaches approximately .6 mach, (60% of the speed of sound) the engine will "top out". Beyond this speed the additional airflow into the motor does not create enough extra power to overcome the pumping losses, and the result is a decrease in horsepower. It should be obvious now that velocity is critical, and must be carefully balanced with airflow. "
 
 

So while my air velocity falls quite short of Mach 0.6, I think the smaller diameter/longer runners did help quite a bit.
FWIW

Ed Anderson
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