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2041 items

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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, Paul
Corporate 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, Eric
Corporate 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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Altitude Effects on Intra-Abdominal Lesions. A. The Effects of Altitude on Induced E. Coli Periontitis in Mice
Author(s): Harridge, William H., Cole, Warren H.
Corporate Author(s): University of Illinois College of Medicine
Date of Publication: 1953-01
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Psychophysiological Effects of Cold I. The Role of Skin-Temperature and Sensory Sensitivity in Manual Performance Decrement
Author(s): McCleary, Robert A.
Corporate Author(s): School of Aviation Medicine
Laboratory: School of Aviation Medicine
Date of Publication: 1953-01
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Physiological Effects of Mechanical Vibration
Author(s): Guillemin, Victor, Wechsberg, Pablo
Corporate Author(s): University of Illinois
Laboratory: School of Aviation Medicine
Date of Publication: 1953-01
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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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