Full-scale span load distribution on tapered wing with split flaps of various spans.

Bibliographic Details
Corporate Author: United States. National Advisory Committee for Aeronautics
Format: Government Document eBook
Language:English
Published: [Washington] : [s.n.], 1937.
Subjects:
Online Access:Electronic resource (PDF)
Description
Item Description:Contains tables, diagrams, images and a list of references.
Physical Description:1 online resource (29 pages), digital, PDF file