Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails : 1. Basic loading condition.

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:Includes reference list of related reports, drawings and graphs.
Physical Description:1 online resource (31 pages), digital, PDF file