DVD 7 - Design Procedures for Engine Cooling

DVD 7 - Design Procedures for Engine CoolingThis DVD discusses the various factors to be considered in obtaining adequate cooling for the engine with a minimum of drag. This is a very important design factor that is not dealt with properly by many texts books. Cooling drag can be as much as 20 percent of the total drag of an airplane. This is real benefit to someone designing an aircraft or wanting to improve an existing design.

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It is important to understand all of the factors that should be considered in determining the wing plan form

tires and tubes

There are literally thousands of reports and test documentation on the characteristics of airfoil shapes

In the past few years’ computer programs have been developed to layout a specific airfoil based upon the desired characteristics the design is to achieve

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aluminum support angles

main gear wheels

For more info

weighing over 2

either for the wing or tail surfaces

vertical and horizontal tips