Effect at high subsonic speeds of fuselage forebody strakes on the static stability and vertical-tail-load characteristics of a complete model having a delta wing, by Edward C. Polhamus et al.

Title:	Effect at high subsonic speeds of fuselage forebody strakes on the static stability and vertical-tail-load characteristics of a complete model having a delta wing
Author:	Polhamus, Edward C.
Author:	Spreemann, Kenneth P.
Author:	Langley Aeronautical Laboratory
Author:	United States. National Adviosry Committee for Aeronautics
Author:	United States. National Advisory Committee for Aeronautics
Note:	National Advisory Committee for Aeronautics, 1958

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Subject:	Airplanes -- Fuselage
Subject:	Airplanes -- Models -- Testing
Subject:	Airplanes -- Tail surfaces
Subject:	Airplanes -- Wings, Triangular
Subject:	Charts, diagrams, etc.
Subject:	Loads (Mechanics)
Subject:	Stability of airplanes, Lateral
Subject:	Stability of airplanes, Longitudinal
Subject:	Wind tunnel testing
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