Effectiveness of an all-movable horizontal tail on an unswept-wing and body combination for Mach numbers from 0.60 to 1.40, by Louis S. Stivers et al.

Title:	Effectiveness of an all-movable horizontal tail on an unswept-wing and body combination for Mach numbers from 0.60 to 1.40
Author:	Stivers, Louis S.
Author:	Ames Research Center
Note:	National Aeronautics and Space Administration, 1959

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Subject:	Aircraft design
Subject:	Angle of attack
Subject:	Body-wing and tail configurations
Subject:	Boundary layer transition
Subject:	Downwash
Subject:	Lift
Subject:	Mach number
Subject:	Pitching moments
Subject:	Stagnation point
Subject:	Tail assemblies
Subject:	Transonic speed
Subject:	Unswept wings
Subject:	Wind tunnel tests
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