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The Planing Characteristics of Two V-Shaped Prismatic Surfaces Having Angles of Dead Rise of 20 and 40
Author(s): Chambliss, Derrill B., Boyd, George M.
Corporate Author(s): Langley Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-01
Report number: NACA TN 2876
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A Rapid Method for Estimating the Separation Point of a Compressible Laminar Boundary Layer
Author(s): Loftin, Lawrence K., Wilson, Homer B.
Corporate Author(s): Langley Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-02
Report number: NACA TN 2892
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Theoretical Calculation of the Pressure Distribution, Span Loading, and Rolling Moment Due to Sideslip at Supersonic Speeds for Thin Sweptback Tapered Wings with Supersonic Trailing Edges and Wing Tips Parallel to the Axis of Wing Symmetry
Author(s): Margolis, Kenneth, Sherman, Windsor L., Hannah, Margery E.
Corporate Author(s): Langley Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-02
Report number: NACA TN 2898
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An Analysis of the Factors Affecting the Loss in Lift and Shift in Aerodynamic Center Produced by the Distortion of a Swept Wing Under Aerodynamic Load
Author(s): Mathews, Charles W., Kurbjun, Max C.
Corporate Author(s): Langley Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-03
Report number: NACA TN 2901
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Matrix Methods for Determining the Longitudinal-Stability Derivatives of an Airplane from Transient Flight Data
Author(s): Donegan, James J.
Corporate Author(s): Langley Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-03
Report number: NACA TN 2902
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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, William
Corporate 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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