The Effect of Initial Curvature on the Strength of an Inelastic Column

Author(s): Mathauser, Eldon E.
Corporate Author: Langley Aeronautical Laboratory
Laboratory: Langley Aeronautical Laboratory
Date of Publication: 1953-01
Report Number: NACA TN 2872

On Traveling Waves in Beams

Author(s): Leonard, Robert W.
Corporate Author: Langley Aeronautical Laboratory
Laboratory: Langley Aeronautical Laboratory
Date of Publication: 1953-01
Report Number: NACA TN 2874

Theoretical Investigation of the Longitudinal Response Characteristics of a Swept-Wing Fighter Airplane Having a Pitch-Attitude Control System

Author(s): Stokes, Fred H.
Corporate Author: Langley Aeronautical Laboratory
Laboratory: Langley Aeronautical Laboratory
Date of Publication: 1953-01
Report Number: NACA TN 2882

Theroetical and Measured Attenuation of Mufflers at Room Temperature without Flow, with Comments on Engine-exhaust Muffler Design

Author(s): Davis, Don D.
Corporate Author: Langley Aeronautical Laboratory
Laboratory: Langley Aeronautical Laboratory
Date of Publication: 1953-02
Report Number: NACA TN 2893

Effect of Thermal Properties on Laminar Boundary-Layer Characteristics

Author(s): Klunker, E. B.
Corporate Author: Langley Aeronautical Laboratory
Laboratory: Langley Aeronautical Laboratory
Date of Publication: 1953-03
Report Number: NACA TN 2916