NACA-TR-460
The characteristics of 78 related airfoil sections from tests in the variable-density wind tunnel
Note:
This document has not been validated by ESDU. It is provided to our users as a useful reference source.
Abstract:
An investigation of a large group of related airfoils was made in the NACA variable-density wind tunnel at a large value of the Reynolds number. The tests were made to provide data that may be directly employed for a rational choice of the most suitable airfoil section for a given application. The variation of the aerodynamic characteristics with variations in thickness and mean-line form were systematically studied. (author)
Author(s):
E.N. Jacobs; K.E. Ward; R.M. Pinkerton
Indexed under:
- None
Details:
NACA-TR-460 | |
---|---|
Format: |
|
Status: |
|
Previous Releases: |
|
The document you have requested is available only to subscribers.
- Subscribers login here.
- If you are not an ESDU subscriber find out how to subscribe.