Starting Propeller sizes are mid range pitch props that should fly just about any plane designed for that size engine. Use these first as in most cases they will be close to being the correct size. Then use trial and error to try and fine tune the maximum performance from your ship by trying the alternate props. If none work better stick with the recommended starting prop
Prop Chart For Two - Stroke Engines
| Engine Size | Starting Prop | Alternate Propellers |
| .20 - .21 | 9x6 | 9x5,10x5 |
| .40 | 11x6 | 10x6,10x7,11x4,11x5.11x7,11x7.5,12x4,12x5 |
| .45 - .48 | 11x6 | 10x6,10x7,10x8,11x7,11x7.5,12x4,12x5,12x6 |
| .60 - .65 | 12x6 | 11x7.5,11x7.75,11x8,12x8,13x5,13x6,14x5,14x6 |
| .80 | 13x6 | 12x8,13x8,14x4,14x6 |
| .90 | 14x6 | 13x6,14x8,15x6,16x6 |
| 1.20 | 16x6 | 14x8,15x6,15x8,16x8,17x6,18x5,18x6 |
| 1.60 | 18x6 | 15x6,15x8,16x8,18x6,18x8,20x6 |
| 2.40 | 18x10 | 18x12,20x8,20x10 |
| 2.70 | 20x8 | 18x10,18x12,20x10 |
| 3.00 | 20x10 | 18x12,20x10 |
Prop Chart For Four - Stroke Engines
| Engine Size | Starting Prop | Alternate Propellers |
| .20 - .21 | 9x6 | 9x5,10x5 |
| .40 | 11x6 | 10x6,10x7,11x4,11x5.11x7,11x7.5,12x4,12x5 |
| .45 - .48 | 11x6 | 10x6,10x7,10x8,11x7,11x7.5,12x4,12x5,12x6 |
| .60 - .65 | 12x6 | 11x7.5,11x7.75,11x8,12x8,13x5,13x6,14x5,14x6 |
| .80 | 13x6 | 12x8,13x8,14x4,14x6 |
| .90 | 14x6 | 13x6,14x8,15x6,16x6 |
| 1.20 | 16x6 | 14x8,15x6,15x8,16x8,17x6,18x5,18x6 |
| 1.60 | 18x6 | 15x6,15x8,16x8,18x6,18x8,20x6 |
| 2.40 | 18x10 | 18x12,20x8,20x10 |
| 2.70 | 20x8 | 18x10,18x12,20x10 |
| 3.00 | 20x10 | 18x12,20x10 |
Another Prop Chart For Two - Stroke Engines
| .049 - .051 | 5.5x4, 5.5x4.5, 6x3, 6x3.5, 6x4 |
| .09 - .10 | 7x3, 7x4, 7x5, 7x6 |
| .15 | 7x6, 8x3, 8x4, 8x5, 8x6, 8x7 |
| .20 - .25 | 8x6, 8x7, 9x4, 9x5 |
| .29 - .35 | 9x6, 9x7, 9x8, 9.5x6, 10x4, 10x5, 10x6 |
| .40 | 9.5x6, 10x4, 10x5, 10x6, 10x7, 10x8, 10x9 |
| .45 - .50 | 10x7, 10x8, 11x4, 11x5, 11x6, 11x7, 11x7.5 |
| .60 | 11x5, 11x6, 11x7, 11x7.5, 11x8, 11x9, 11x10 |
| .71 - .80 | 12x6, 12x8, 13x6, 13x8, 13x10, 14x8 |
| .90 | 13x6, 13x8, 13x10, 14x6, 14x8 |
| 1.08 | 14x8, 15x8, 16x6 |
| 1.20 | 14x8, 15x8, 16x6 |
| 1.5 | 16x8, 16x10, 18x6, 18x8 |
| 1.8 | 18x8, 18x10, 20x6, 20x8 |
| 2.1 | 20x8, 20x10 |
| 2.7 - 3.5 | 22x8, 22x10, 22x12, 24x8, 24x10, 24x12 |
B. General Information about Propellers
Propellers are an all-important part of airplanes to provide the necessary
thrust for powered flight. Even our jet engines have bypass blades to assist in
producing thrust. In the simplest terms, a propeller is an airfoil traveling in
a circle with a positive angle of attack relative to the incoming air to produce
thrust.
Propeller performance is affected by several factors, among them are diameter
relative to RPM, and blade area relative to power absorption and pitch.
Diameter is the measurement (usually in inches) of the prop from tip to tip.
Pitch is defined as the theoretical advancement of a propeller in one revolution
(usually measured in inches) and defines the speed and maneuverability
characteristics of flying. For example, a 10x6 describes a diameter of 10"
and a pitch of 6", or forward movement of 6 inches per revolution. In
metric measurement this would be 30x15. Sometimes a particular series letter is
used, such as 1260S (12" diameter, 6" pitch, Scimitar Series).
Now, more about pitch, which is the hardest part to visualize. Imagine you turn
a 6" pitch prop in a tub of something like butter. It should advance
6" for each turn along its axis. Naturally, the faster you turn the prop,
the more rapidly you will advance. Model propellers have a practical limit on
how fast they can turn (RPM) based on the power curve of the engine and the
diameter of the prop. Another practical limit is due to noise considerations.
Prop tip speed limits should be at 600 to 650 feet per second. Tip speed is
explained below.
Slow speeds, aerobatics, great take-off's and landings can all be accomplished
with low pitch propellers. Higher pitches lead to less maneuverable but faster
flying. Because modelers do not have the luxury of variable pitch, most select a
pitch based on how they like to fly or compromise speed and maneuverability with
a pitch somewhere in the middle - around 65 -70% of the prop diameter. A
limiting factor which will decrease propeller efficiency is engine horsepower
and aircraft drag, i.e. a high pitch prop can't make an airplane any faster than
it's capable of being and too low of pitch can result in lower power/thrust. It
should be noted that industry standards are that pitch is measured at 75% of
radius.
Thrust refers to the force exerted by the rotating propeller in the direction of
travel of the airplane. This is the whole purpose of the propeller - to convert
the power of the engine which appears as a rotating force, or torque, into a
linear force to propel the airplane. Thrust is usually measured in pounds is a
function of air density, rpm, diameter, advance ratio and Reynolds number. It is
a long, complicated process to get this number, but what is important to
remember is that thrust is different for every shape of propeller and changes
with flying conditions.
Power Absorption refers to the power output curve of the engine. Power is the
product of torque times rpm. As rpm increases, an engine produces less force (or
torque) because the air/fuel mixture is not as efficient at higher rpm's. This
is why a power curve becomes flat or decreases at higher rpm's, and means that
the most efficient propeller is the one that allows the engine to operate at its
optimum power band.
An interesting point in understanding power absorption is that propeller power
varies as the cube of the rpm. Consequently, twice the rpm requires 8 times the
power.
Tip Speed is measured in feet per second and a formula is provided below to find
this measurement.
For model airplane purposes, the best tip speed for efficiency and noise
requirements is 600 feet per second. This is due to compressibility losses and
the fact that subsonic airfoils do not work well in transonic/sonic speeds with
required sound levels.
Feet Per Second (ft/s) = RPM x diameter in inches x .00436For example, to find the tip speed of a 10x6 on a .40 size engine running at 13,500 RPM, the equation would be 13,500 x 10 x .00436 = 588.6 ft/s.
Diameter in inches = 138,000 / RPM
Using a .40 engine running at 13,500 RPM,
the equation would read as follows:
138,000/13,500 = 10.22
Rounding down, the correct diameter is 10"
For both of the above formulas, use RPM for the optimum power band of your
engine. Consult your owner's manual if you do not know this number.
C. RPM Operating Limits -
One of the differences between wood and glass-filled nylon propellers is that
glass-filled nylon props have suggested RPM limits for mechanical
considerations. This will vary according to diameter. For Master Airscrew props,
we suggest the following formula: RPM Operating Limit = 160,000 divided by
Diameter in inches. In our .40 size engine example, a 10" diameter g/f
nylon prop has an operating limit of 16,000 rpm, well above the requirement of a
.40 engine.
D. Gearbox Ratio Recommendations -
Wingspan smaller than 2 meters:
Wingspan at 2 meters:
Wingspan larger than 2 meters: