Calculation of chord-wise load distribution over air℗-foil sections with plain, split, or serially hinged trailing℗--edge flaps.

Bibliographic Details
Corporate Author: United States. National Advisory Committee for Aeronautics
Format: Government Document eBook
Language:English
Published: [Washington] : [s.n.], 1938.
Subjects:
Online Access:Electronic resource (PDF)
Description
Item Description:Includes tables and graphs.
Physical Description:1 online resource (24 pages), digital, PDF file