Side forces on a tangent ogive forebody with a fineness ratio of 3.5 at high angles of attack and Mach numbers from 0.1 to 0.7 / Earl R. Keener [and others]

Saved in:

Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Corporate Author:	United States. National Aeronautics and Space Administration
Other Authors:	Keener, Earl R.
Format:	Government Document Book
Language:	English
Published:	Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977.
Series:	NASA technical memorandum ; X-3437.
Subjects:	Stability of airplanes, Lateral. Aerodynamic load. Noses (Aircraft) > Testing. Spin (Aerodynamics) Yawing (Aerodynamics)

Internet

Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.15:3437
NAS 1.15:3437	Available Place a Hold