The following results were derived from Computational Fluid Dynamics testing. A model of a Cessna 172
wing was built in a CFD computer.  All testing was conducted on an eight foot section of the wing with a
three degree angle of attack. The following graph shows the total amount of lift produced over the wing
section at various wind speeds. The red line indicates the total amount of lift produced by the wing before
the AeroSpoiler  was installed. The green line indicated the total lift produced over the same wing section
with the AeroSpoiler installed. These tests were conducted at wind speeds of 50, 100, 150 and 200 MPH.

  The AeroSpoiler has undergone extensive design, environmental and
structural testing.  All components of the AeroSpoiler have been       
                 designed, engineered and manufactured to exceed design specifications.       

1) Design Testing:

     The AeroSpoiler was designed using Computational Fluid Dynamics Testing (CFD).

     An independent design engineer and CFD specialist was used to perform all CFD testing for this product.

     CFD testing allowed us to receive very accurate results while maintaining very precise parameters.

     The AeroSpoiler was tested with wind speeds up to 200 MPH. 

     Results of CFD testing were used to determined the type and dimensions of the materials required for the
     AeroSpoiler to perform properly.

     Results of CFD testing show that the AeroSpoiler will reduce the lift producing capability of a wing by
     as much as 96%  at 50MPH and 92% at 200MPH over the area of the wing where the AeroSpoiler is
     installed.

2) Structural Testing:

     Structural testing was conducted on the AeroSpoiler to ensure that each component met the specified
     design requirements.

     Stress analysis and durability testing was performed on each component as necessary. 

3) Environmental Testing:

     Environmental testing was conducted to ensure that the AeroSpoiler would survive in the worst of
     weather conditions.

     As a result of this testing all internal components of the AeroSpoiler are stainless steel. Stainless steel
     parts assure that the AeroSpoiler will function properly without any concerns for rust or corrosion.

     The Cup/Receiver assembly is constructed with a very strong and durable injection molded ABS plastic.
     The ABS is colored before it is molded allowing for the assembly to retain it's original color for many 
     years.  ABS plastic is corrosion proof and rust resistant.

     The Blades are cut from 5/16th inch PVC sheets. These sheets are also solid red and UV coated to allow 
     them to retain there original color longer.  PVC is also a corrosion proof and rust resistant material.

     Note:  Please be aware that over time ultra violet rays from the sun will cause the color to fade on both 
                 the blades and the receivers.

     Note:  The AeroSpoiler should not be used in temperatures below freezing. The cups will freeze to the 
                 wing surface and may cause damage to your aircraft when trying to remove them.


                                          US Patent Pending