Wind-tunnel investigation of the aerodynamic characteristics in pitch and sideslip at high subsonic speeds of a wing-fuselage combination having a triangular wing of aspect ratio 4, by Paul G. Fournier et al.

Title:	Wind-tunnel investigation of the aerodynamic characteristics in pitch and sideslip at high subsonic speeds of a wing-fuselage combination having a triangular wing of aspect ratio 4
Author:	Fournier, Paul G.
Author:	Langley Aeronautical Laboratory
Author:	United States. National Adviosry Committee for Aeronautics
Note:	National Advisory Committee for Aeronautics, 1953

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Subject:	Airplanes -- Wings, Swept-back
Subject:	Airplanes -- Wings, Triangular
Subject:	Charts, diagrams, etc.
Subject:	Leading edges (Aerodynamics)
Subject:	Pitching (Aerodynamics)
Subject:	Rolling (Aerodynamics)
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