Contrails
The goal of the Contrails project is to help preserve and disseminate the technical record of 20th century aerospace research, highlighting in particular the research endeavors of the Illinois Tech community.

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5 reports

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: 1/1/1953
Report Number: NACA TN 2872
full text unavailable

On Traveling Waves in Beams

Author(s): Robert W. Leonard; Bernard Budiansky
Corporate Author: Langley Aeronautical Laboratory
Laboratory: Langley Aeronautical Laboratory
Date of Publication: 1/1/1953
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): Fred H. Stokes; J. T. Matthews
Corporate Author: Langley Aeronautical Laboratory
Laboratory: Langley Aeronautical Laboratory
Date of Publication: 1/1/1953
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): Don D. Davis; George L. Stevens, Dewey Moore, George M. Stokes
Corporate Author: Langley Aeronautical Laboratory
Laboratory: Langley Aeronautical Laboratory
Date of Publication: 2/1/1953
Report Number: NACA TN 2893
full text unavailable

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: 3/1/1953
Report Number: NACA TN 2916
full text unavailable