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Evaluation of Gust Response Characteristics of Some Existing Aircraft with Wing Bending Flexibility Included
Author(s): Kordes, Eldon E., Houbolt, John C.
Corporate Author(s): Langley Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-02
Report number: NACA TN 2897
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Theroetical and Measured Attenuation of Mufflers at Room Temperature without Flow, with Comments on Engine-exhaust Muffler Design
Author(s): Davis, Don D., Stevens, George L., Moore, Dewey, Stokes, George M.
Corporate Author(s): Langley Aeronautical Laboratory
Laboratory: Langley Aeronautical Laboratory
Date of Publication: 1953-02
Report number: NACA TN 2893
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Effect of Thermal Properties on Laminar Boundary-Layer Characteristics
Author(s): Klunker, E. B., McLean, F. Edward
Corporate Author(s): Langley Aeronautical Laboratory
Laboratory: Langley Aeronautical Laboratory
Date of Publication: 1953-03
Report number: NACA TN 2916
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A Study of the Application of Power-Spectral Methods of Generalized Harmonic Analysis to Gust Loads on Airplanes
Author(s): Press, Harry, Mazelsky, Bernard
Corporate Author(s): Langley Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-01
Report number: NACA TN 2853
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Estimated Power Reduction by Water Injection in a Nonreturn Supersonic Wind Tunnel
Author(s): Cooper, Morton, Sevier, John R.
Corporate Author(s): Langley Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-01
Report number: NACA TN 2856
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The Effect of Initial Curvature on the Strength of an Inelastic Column
Author(s): Mathauser, Eldon E., Brooks, William, Wilder, Thomas W.
Corporate Author(s): Langley Aeronautical Laboratory
Laboratory: Langley Aeronautical Laboratory
Date of Publication: 1953-01
Report number: NACA TN 2872
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On Traveling Waves in Beams
Author(s): Leonard, Robert W., Budiansky, Bernard
Corporate Author(s): Langley Aeronautical Laboratory
Laboratory: Langley Aeronautical Laboratory
Date of Publication: 1953-01
Report number: NACA TN 2874
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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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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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