A Concise Theoretical Method for Profile-Drag Calculation: Advance Report
Price not available for France
You can still browse on Amazon. Try another country above.
Book Details
Ratings & Reviews
No reviews yet — be the first!
No reviews yet.
Description
In this report a method is presented for the calculation of the profile drag of airfoil sections. The method requlres only a knowledge of the theoretical velocity distribution and can be applied readily once this dlstribution is ascertained. Comparison of calculated and experimental drag characteristics for several airfoils shows a satisfactory agreement. Sample calculatlons are included.
