Free-spinning wind-tunnel tests of low-wing monoplane with systematic changes in wings and tails, III. Mass distributed along the wings.

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 illustrations and list of references.
Physical Description:1 online resource (30 pages), digital, PDF file