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

Author(s): Eldon. E. Mathauser; William Brooks; Thomas W. Wilder
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): Robert W. Leonard; Bernard Budiansky
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): Fred H. Stokes; J. T. Matthews
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): Don D. Davis; George L. Stevens, Dewey Moore, George M. Stokes
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): E. B. Klunker; F. Edward McLean
Corporate Author: Langley Aeronautical Laboratory
Laboratory: Langley Aeronautical Laboratory
Date of Publication: 1953-03
Report Number: NACA TN 2916