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, by Earl R. Keener et al.

Title:	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
Author:	Keener, Earl R.
Author:	United States. National Aeronautics and Space Administration
Note:	National Aeronautics and Space Administration ;, 1977

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Subject:	Aerodynamic load
Subject:	Noses (Aircraft) -- Testing
Subject:	Spin (Aerodynamics)
Subject:	Stability of airplanes, Lateral
Subject:	Yawing (Aerodynamics)
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