Flying faster on the same power - reducing cooling drag



About the Benefits
  • Overview
  • Getting rid of the heat
  • Heat - the top end killer
  • More power per cubic inch
  • Better performance and fuel economy
  • Radiator technology - past and present
  • Shock cooling - Problem solved!
  • The secret to achieving longer TBOs
  • Flying faster on the same power - reducing cooling drag
  • Side benefits - Safer cabin heat
  • Dispelling the Myths



  • The title of this section says it all. There are two ways we can fly faster, either develop more power or reduce the airframe drag. Today's air-cooled engines require a substantial volume of airflow that must be passed over a large and complex structure. Passing this much air past such a complex structure as an engine creates drag and that drag adds to the overall parasitic drag of the airframe. This type of drag call cooling drag. In addition it is very difficult to get the airflow over the engine to pass evenly by each of the cylinders. The result is eneven cooling of the cylinders with the front cylinders generally running much hotter than the rear cylinders. Using an air-cooled engine means that there are few options on how to pickup cooling air and were the heated waste air can be dumped.

    A liquid cooled engine offers several benefits to reduce cooling drag. The first benefit is that we now only need sufficient airflow to pass over a high density radiator. Such a radiator is designed to provide substantially more thermal conductivity thereby reducing the amount of air required to remove the same amount of heat. A radiator can be located in more aerodynamically suitable locations on the airframe. Air pickup can also be located in more optimum locations and internal ducting offers the opportunity to create a far more efficient air stream to the radiator. Slowing the incoming cooling air and allowing it to expand towards the radiator surface allows much more efficient cooling. More heat is dissipated to a smaller air volume.

    A radiator presents far less drag on the passing air flow than does a complex structure such as an engine with baffles. Reducing the air flow volume while at the same time reducing the drag as the air passes thru the radiator means an overall reduction in cooling drag.

    It used to be that the convention wisdom was that a low drag radiator with a reduced number of fins per inch was the most aerodynamically efficient way to reduce cooling drag. This allowed a high volume of high speed air to pass through the radiator with little pressure differential (aka drag). Today we have learned through high speed automotive racing that the opposite is true. It is better to have a small volume of air passing at relatively low speed through a highly efficient radiator structure (ie: high pressure differential across the radiator) and to allow the incoming air to back up at the air inlet.

    The result of this approach is that a far smaller air inlet is required and that the smaller volume airstream carries off far more waste heat. The smaller volume of air is handling a higher heat load. It also means that the cooling air inlet can be located in shaped in such a manner as to take advantage of the pressure dome that will be created at the inlet. This pressure dome can be viewed as almost a flat surface which can be blended into the surrounding structure to produce a smooth aerodynamic contour. The overall result is substantially reduced cooling drag.

    The much more efficient radiator also means that far less airflow is required for cooling on the ground - reducing the need for supplemental boost fans in most installations.



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    Proudly MADE in the U.S.A.