Fuselage-drag tests in the variable-density wind tunnel : Streamline bodies of revolution, fineness ratio of 5.

Bibliographic Details
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document eBook
Language:	English
Published:	[Washington] : [s.n.], 1937.
Subjects:	Aerodynamics. Airplanes. Aeronautics > Research. Mathematical models.
Online Access:	Electronic resource (PDF)

Description
Item Description:	Includes 3 tables. Also includes reference list of related reports.
Physical Description:	1 online resource (26 pages .), digital, PDF file