Article navigation

IT is wished to propose a simple graphical method for finding the approximate C.P. position of an aerofoil directly from the CL (CM) curve in cases where the C.P. positions are not indicated—as, for instance, in the American and British aerofoil data reports. This method eliminates the necessity of calculating for each CL the a by the well known relation

This content is only available via PDF.
You do not currently have access to this content.
Don't already have an account? Register

Purchased this content as a guest? Enter your email address to restore access.

Pay-Per-View Access
$39.00
Rental

or Create an Account

Close Modal
Close Modal