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204 items

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Theoretical Investigation of the Longitudinal Response Characteristics of a Swept-Wing Fighter Airplane Having a Pitch-Attitude Control System
Author(s): Stokes, Fred H., Matthews, J. T.
Corporate Author(s): Langley Aeronautical Laboratory
Laboratory: Langley Aeronautical Laboratory
Date of Publication: 1953-01
Report number: NACA TN 2882
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Reflection of Weak Shock Wave from a Boundary Layer Along a Flat Plate. II. Interaction of Oblique Shock Wave with a Laminar Boundary Layer Analyzed by Differential-Equation Method
Author(s): Kuo, Yung-Huai
Corporate Author(s): Cornell University
Date of Publication: 1953-01
Report number: NACA TN 2869
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Bearing Strengths of Some 75S-T6 and 14S-T6 Aluminum-Alloy Hand Forgings
Author(s): Finley, E. M.
Corporate Author(s): Aluminum Company of America
Date of Publication: 1953-01
Report number: NACA TN 2883
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Calculation and Measurement of Normal Modes of Vibration of an Aluminum-Alloy Box Beam with and without Large Discontinuities
Author(s): Smith, Frank C., Howard, Darnley M.
Corporate Author(s): National Bureau of Standards
Date of Publication: 1953-01
Report number: NACA TN 2884
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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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Calculation of the Shape of a Two-Dimensional Supersonic Nozzle in Closed Form
Author(s): Cunsolo, Dante
Date of Publication: 1953-01
Report number: NACA TM 1358
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Effects of Hypothermia on Brain Activity
Author(s): Noell, Werner K., Briller, Stanley A.
Corporate Author(s): Department of Neuropsychiatry
Laboratory: School of Aviation Medicine
Date of Publication: 1953-01
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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-Huai
Corporate 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, 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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