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Effect of Horizontal-Tail Span and Vertical Location on the Aerodynamic Characteristics of an Unswept Tail Assembly in Sideslip
Author(s): Riley, Donald R.Corporate Author(s): Langley Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-03
Report number: NACA TN 2907
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An Application of the Method of Characteristics to Two-Dimensional Transonic Flows with Detached Shock Waves
Author(s): Harder, Keith C., Klunker, E. B.Corporate Author(s): Langley Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-03
Report number: NACA TN 2910
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A Low-Speed Experimental Study of the Directional Characteristics of a Sharp-Nosed Fuselage Through a Large Angle-of-Attack Range at Zero Angle of Sideslip
Author(s): Letko, WilliamCorporate Author(s): Langley Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-03
Report number: NACA TN 2911
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