Two-Stroke Software Review

Part 1 - Introduction to Two-Stroke Software

Bimotion v 2.1 - Blair S.A.E. - Dynomation 2 - MOTA v 5.0 - TSR


Using MOTA v 5.0


1989 Blaster Engine Rebuild

Using MOTA v 5.0
One of the key features of MOTA 5 is that it can run engine simulations. It will display the engine graphically. It will allow a set of performance curves to be plotted as graphs with engine power and torque at an engine speed. The dynamic wave display allows a visual of the propagation of pressure, velocity, temperature, density and the purity of waves in each duct. This includes the exhaust pipe. Additional selections allow simulations of the reed or rotary valve at speed. Output data shows the cylinder, exhaust pressure difference and the scavenging ratio, complete with delivery ratios, power and torque, BMEP, PMEP, FMEP, IMEP, brake specific fuel consumption, flow ratios - the delivery and exhaust gas ratios, the mass based scavenge ratio, the volume based scavenge ratio, scavenging efficiency, the percentage of energy lost due to heat through the exhaust and the peak cylinder temperature and pressure.
 
The MOTA 5 programs allow the design of engines parameters when the input is entered in metric units of measurement. The selections from the menu and submenu's are:
 
Create or Edit an Engine Data File
 
Run MOTA - The Engine Simulator
 
Display Output Graphics
 
View an Engine Specification and Performance File
 
Performance Curves Calculator
 
Expansion Chamber Cone Construction
 
Within the software is a section called dimensioning utilities. It is very helpful when trying to determine some of the more unusual engine parameters. For instance if you know the piston pin is offset 1 mm in the positive direction (toward the direction of engine rotation) the program will calculate where BDC is - in this case 180.29 degrees ATDC. Offset the piston pin another mm and BDC moves to 180.58 degrees ATDC. Isn't it interesting to know that small changes in the offset of the piston pin can have a noticeable effect upon where these positions end up.
 
There are some terms which may need clarifying, for example - the volume of the combustion chamber when the piston is at top dead center is referred to as Cylinder Clearance Volume. The Crankcase Clearance Volume is defined as being the volume below the piston crown when the piston is at BDC. MOTA will allow the design of engines that are either piston port, rotary valve or have reed valves. For reed valve engines there is input for reed petal thickness and type of material as well as whether the thickness is constant over the total length of the petal, the width, unclamped pedal width and density of the petal material. There is also input pertaining to the values of Young's Modulus and for reed petals that overlap one another (Boyesen). The reed valve block is broken down into several more specific dimensions for precise data entry. This includes the number of ports, block angle, width of each port, corner radii, length of port and the stop plate radius. The term "tip deflection" refers to the amount of distance a reed petal can open. For disc valve equipped engines there is input for the opening, closing, height, width, corner radius and radius to the bottom of the port. MOTA uses what is called Fuel Calorific Value. This relates to the octane of the gasoline used in the design. This value is set as a default to 98 octane leaded gasoline. There is input for different air/fuel ratios at different engine operating speeds.
 
Transfer port input is classified as the number and type of duct. There is input for the transfer duct dimensions. There can be as many as 3 pair of transfer ports and 1 additional (boost) port. There is input data describing the sectional area of these passages. Engine port dimensions are entered after measuring them using one of the methods available. This can be as simple as knowing the port height, width and top and bottom corner radius. Additional port dimensions can be entered using what is called profiled data. This is defined as entering a port shape with as many as ten different intervals (sections) associated with the port width. Here you can enter bridged ports and auxiliary exhaust ports (finger ports). The term Axial Attitude Angle refers to the port roof angle. The term Radial Attitude Angle refers to the way vertical port walls are recorded. It is different than the way other software programs determine it. The scavenging cycle is given particular attention and is described as having one of four different characteristics. Inlet duct dimensions may have data entered in as few as 2 and as many as 4 sections. These sections are described as being the inlet pipe sections. This includes any section after the carburetor bell mouth and may have its parameters entered as length, diameter of inlet and diameter of outlet.
 
MOTA has an input category to simulate the engine whether it is equipped with an exhaust control valve or not. Additionally, it asks for the number of sections the tuned exhaust pipe has which is fitted to it. For simulation, the exhaust pipe data entry is input in as many sections as necessary to accurately describe the pipe - this includes section length and width. When I entered my data I subtracted the thickness of the pipe material to keep the dimensions tight. As a separate design parameter there are input for 2 different types of mufflers, classified as integrated or separate. Integrated mufflers are those that more closely comply to pipes with internal stingers. I choose a separate muffler for my engine. Ignition and combustion efficiency are represented and described in degrees of crankshaft rotation. There is input to change the ignition timing (advance or retard) of an engine at different operating speeds.
 
The MOTA 5 simulator is unlike the Dynomation 2 simulator in that it does not display a graph as the data is run through the simulation process. Its information appears on the screen as numbers within columns. This method of display, though not as visually appealing is less confusing because there is much less activity on the screen. The hard data is displayed without any bells or whistles. My initial simulation run(s) indicate a decrease of power during the 40 run set - I suspect this is due to heat. The power (13 hp) at 5000 was slightly higher than it was at 4000 RPM as is the mean exhaust temperature - it's simulated at 1092 degrees. After the first 2 sets of runs (4000 RPM & 5000 RPM) the screen displayed a couple of graphs which indicate the power/torque and peak cylinder temperature and pressure. At 6000 RPM power is up to 18 hp and the exhaust temperature is down about 100 degrees. At 7000 RPM again power is up. This time it shows 24 HP with an exhaust temp of 1038 degrees. At 8000 its reading 24.6 HP and the exhaust is 1047. At 9000 power falls off to 21 HP with the exhaust temperature of 1050. It made me want to try a leaner fuel to air ratio - I think power would be increased. Currently the fuel mixture is set at 12:1. I altered the fuel mixture and ignition timing in the examples below to indicate the changes MOTA 5 can do. The values are listed like this ... RPM = HP (Exhaust gas temperature). Peak power is indicated in red.
 
Update 9/18/99 - As usual an enthusiast pointed out a serious error I have made while doing this testing. This one comes from a man named Steve who reminded me that changing the fuel mixture in the direction I indicate below is making the mixture RICHER not leaner. So it seems the richer I made the mixture the more power the simulated engine made. I'll have to re-run the simulator in the leaner direction (this time for sure) and see what my outcome is. Thanks Steve :)
 
Baseline settings - 12:1 fuel mixture, ignition timing set at 10 degrees BTDC - 5000 = 13 (1092), 6000 = 18 (997), 7000 = 24 (999), 8000 = 24.6 (1038), 9000 = 21 (1050).
 
Lean the mixture from 12:1 to 11.8:1 - 5000 = 15 (937), 6000= 19.6 (947), 7000 = 26.5 (950), 8000 = 26.44 (980), 9000 = 21.1 (958)
 
Changed fuel mixture to 11.4:1 - 5000 = 18.59 (1005), 6000 = 20.3 (969) 7000 = 27.25 (982), 8000 = 28.22 (1014), 9000 = 25.25 (1001)
 
Changed fuel mixture to 11:1 - 5000 = 19.6 (1082), 6000 = 20.82 (992) , 7000 = 28.09 (1005), 8000 = 29.48 (1044), 9000 = 25.8 (1035)

Changing the combustion burn period to 50 degrees of crankshaft rotation (from 55 degrees). Fuel mixture 11:1. 5000 = 20.05 (1084), 6000 = 21.3 (1008), 7000 = 28.77 (991), 8000 = 30.10 (1026), 9000 = 25.8 (1017)

Changed the combustion efficiency to .82 from .85. Fuel mixture 11:1 - 5000 = 19.53 (1075) - peak temps very high (1260), 6000 = 20.9 (951) canceled.

Changed ignition timing to 15 BTDC. Fuel mixture 11:1. Burn period changed back to 55 degrees - 5000 = 20.6 (1078), 6000 = 22.1 (958), 7000 = 29.71 (967), 8000 = 30.28 (986), 9000 = 25.2 (945)

Changed timing to 17.5 BTDC and 11:1 fuel mixture. Burn period 55 degrees - 5000 = 20.94 (1074), 6000 = 22.5(941), 7000 = 30.3 (943), 8000 = 30.4 (971), 9000 = 24.86 (950)

Timing set back to 12 degrees BTDC. Fuel mixture 11:1 - 5000=19.37(1115), 6000= 19.9(987), 7000= 26.2(992), 8000= 29.94 (1041), 9000= 26.71 (970)

It will be interesting to see how this engine does on a real dynamometer. It's hard not to notice that pressing a few keys to change the ignition timing and jetting is much faster and simpler than actually changing the parts on the real engine. As I changed the timing and other variables, I was able to increase the power output. The most noticeable change in power is before and after the power peak.

More to come - Rick

 

Two-Stroke Software Review

Part 1 - Introduction to Two-Stroke Software

Bimotion v 2.1 - Blair S.A.E. - Dynomation 2 - MOTA v 5.0 - TSR


Using MOTA v 5.0


1989 Blaster Engine Rebuild
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Date Last Modified: 9/5/99
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