Pressure-Distribution Investigation of an N.C.A.A. 0009 Airfoil with a 30-Percent Chord Plain Flap and Three Tabs, May 1940.

Bibliographic Details
Format: Government Document eBook
Language:English
Published: [Washington] : [s.n.], 1940.
Subjects:
Online Access:Electronic resource (PDF)
Description
Item Description:Includes tables and formulas.
Physical Description:1 online resource ('14 pages), digital, PDF file