Effects of wing position and vertical-tail configuration on stability and control characteristics of a jet-powered delta-wing vertically rising airplane model, by Powell M. Lovell et al.

Title:	Effects of wing position and vertical-tail configuration on stability and control characteristics of a jet-powered delta-wing vertically rising airplane model
Author:	Lovell, Powell M.
Author:	Parlett, Lysle P.
Author:	Langley Aeronautical Laboratory
Author:	United States. National Advisory Committee for Aeronautics
Note:	National Advisory Committee for Aeronautics, 1957

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Subject:	Airplanes -- Control
Subject:	Airplanes -- Models -- Testing
Subject:	Airplanes -- Tail surfaces
Subject:	Airplanes -- Wings, Triangular
Subject:	Stability of airplanes
Subject:	Vertically rising aircraft -- Handling characteristics
Subject:	Wind tunnel testing
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