Has anyone ever put the prop arc part way through a wing?
[ This would require a slot completely through the wing ] Mine will end up at about
80-90% of the center section airfoil's chord.
From : Don Stackhouse
You can usually get away with this on models, although it hurts the prop
efficiency, and it can generate a fair amount of aerodynamic vibration,
because of the discontinuous, disrupted airflow into the prop.
On full scale aircraft the same issues exist, only their severity and their
potential consequences generally become much more severe. In particular,
the vibrational stresses in the propeller blades can easily be severe
enough to cause fatigue failures in the blades. Losing a propeller blade,
even on the ground, is NOT something you even want to think about! The
problem of the broken blade flying off through surrounding airframe and
occupants is not the biggest problem. Generally the loss of a blade results
in the rest of the prop and engine being ripped completely out of the
airplane by the massive unbalance. The centrifugal force on a typical metal
propeller blade for a light aircraft is around 40,000 to 50,000 pounds.
Even a wooden or composite propeller blade has centrifugal forces of about
half that value, still more than enough to overstress most engine mounts.
Even if the engine stays at least partially attached, it may get bent
around sideways to the airflow, causing massive amounts of drag as well as
possible control problems.
Even on a model, the centrifugal forces can be considerable. In giant scale
models for example, the centrifugal force per blade can be in excess of
several hundred pounds.
I'm thinking of hinging the part behind this slot and using it as a trim tab/elevator.
Anyone had experiances w/ this?
Lifting surfaces, especially control surfaces, located in close proximity
to a prop will tend to skew the airflow into the prop even more. This
increases the vibration and fatigue stresses, and worsens the efficiency
losses.
On a model it's usually possible to pack enough raw power into the aircraft
to overcome the efficiency losses, and the flight time that models
accumulate is generally not enough (usually!) to cause fatigue problems.
However, fixing a poor design by increasing the engine size will increase
weight, which increases the required power, which increases the weight even
more, in a vicious cycle. While the end result may fly OK, it will not fly
as well as a design that uses the capabilities of the motor and prop more
efficiently.
Don Stackhouse
DJ Aerotech
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