Effect of propeller slipstream on wing and tail.

Bibliographic Details
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document eBook
Language:	English
Published:	[Washington] : [s.n.], 1938.
Subjects:	Jet planes. Aeronautics > Research. Mathematical models.
Online Access:	Electronic resource (PDF)

Description
Item Description:	Includes tables, graphs, drawn and photo illustrations.
Physical Description:	1 online resource (60 pages), digital, PDF file