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41 items
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On the Stability of the Laminar Mixing Region Between Two Parallel Streams in a Gas
Author(s): Lin, C. C.Corporate Author(s): Massachusetts Institute of Technology
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-01
Report number: NACA TN 2887
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Reflection of a Weak Shock Wave from a Boundary Layer Along a Flat Plate. I. Interaction of Weak Shock Waves with Laminar and Turbulent Boundary Layers Analyzed by Momentum-Integral Method
Author(s): Ritter, Alfred, Kuo, Yung-HuaiCorporate Author(s): Cornell University
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-01-27
Report number: NACA TN 2868
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The Effect Longitudinal Stiffeners Located on One Side of a Plate on the Compressive Buckling Stress of the Plate-Stiffener Combination
Author(s): Seide, PaulCorporate Author(s): Langley Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-01
Report number: NACA TN 2873
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Behavior in Pure Bending of a Long Monocoque Beam of Circular-Arc Cross Section
Author(s): Fralich, Robert W., Mayers, J., Reissner, EricCorporate Author(s): Langley Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-01
Report number: NACA TN 2875
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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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Factors Affecting Laminar Boundary Layer Measurements in a Supersonic Stream
Author(s): Blue, Robert E., Low, George M.Corporate Author(s): Lewis Flight Propulsion Laboratory
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-02
Report number: NACA TN 2891
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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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Calculations of Upwash in the Region Above or Below the Wing-Chord Planes of Swept-Back Wing-Fuselage-Nacelle Combinations
Author(s): Rogallo, Vernon L., McCloud, John L.Corporate Author(s): Ames Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-02
Report number: NACA TN 2894
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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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The Calculation of Pressure on Slender Airplanes in Subsonic and Supersonic Flow
Author(s): Heaslet, Max A., Lomax, HarvardCorporate Author(s): Ames Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-03
Report number: NACA TN 2900
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