5 reports
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
full text unavailable
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
full text unavailable
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
full text unavailable
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
full text unavailable
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
full text unavailable