Stability and control characteristics of a monoplanar missile configuration with two low-profile tail arrangements at Mach numbers from 1.70 to 2.86, by A. B. Blair et al.

Title:	Stability and control characteristics of a monoplanar missile configuration with two low-profile tail arrangements at Mach numbers from 1.70 to 2.86
Author:	Blair, A. B.
Author:	United States. National Aeronautics and Space Administration
Note:	National Aeronautics and Space Administration ;, 1977

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Subject:	Aerodynamic characteristics
Subject:	Control stability
Subject:	Guided missiles -- Control systems
Subject:	Lift drag ratio
Subject:	Missile design
Subject:	Aerodynamics, Supersonic
Subject:	Supersonic wind tunnels
Subject:	Tail assemblies
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